19–22 August 2019
JW Marriott, Indianapolis, Indiana

Call for Papers

POWERING A CHANGING WORLD 

This is a dynamically shifting time for power and energy systems that mobilize space and aeronautical vehicles. New paradigms in the propulsion field and operational efficiency are upon us, including in the areas of electric aircraft, hybrid rockets, automation, robotics, and hypersonics. The tipping point for these technologies to become a reality and be fully implemented is near.

In addition to the historically strong propulsion and energy topics, the 2019 forum will also offer: (Includes topics from the AIAA Space Technical Community in 2019)

  • Enhanced space content, from cislunar space to small satellites to space architecture
  • Executive-level focus on space propulsion, energy science, air-breathing propulsion, electric propulsion, and more
  • Celebration of the 50th anniversary of the Apollo 11 lunar landing with special exhibits on the Apollo-era technologies and systems

SHARE YOUR RESEARCH WITH YOUR PEERS

Researchers and scientists are invited to take advantage of this opportunity to share and collaborate on the latest research, theory, and technology surrounding aerospace energy and propulsion systems. Attendees consistently state that the greatest value they realize at this forum is the connections they make and the free flow of innovative ideas that come with a focused gathering of their peers. 

Dates to Remember

  • Abstract Submission Opens: 23 October 2018 
  • Abstract Submission Closed: 31 January 2019, 2000 hrs Eastern Time
  • Manuscript Deadline: 15 July 2019, 2000 hrs Eastern Time 
     

Submit A Paper

Student Paper Competition: Additional Information

Suggest a Topic

Abstract Submission Policies Abstract Submission Procedures Abstract Submission Requirements



Go to: Additive Manufacturing for Propulsion Systems
Go to: Advanced Integrated Intelligent Propulsion Controls 
Go to: Advanced Mechanical Components
Go to: Advanced Propulsion Concepts  
Go to: Advanced Vehicle Systems
Go to: Aerospace Power Systems
Go to: Electric Propulsion
Go to: Electricity Delivery and Grid Reliability
Go to: Energetic Components and Systems
Go to: Energy Conversion Technology
Go to: Energy-Efficient and Renewable Energy Technologies
Go to: Fuel and Power Generation Technology 
Go to: Gas Turbine Engines
Go to: High-Speed Air-Breathing Propulsion
Go to: Hybrid Rockets
Go to: Inlets, Nozzles, and Propulsion Systems Integration  
Go to: ITAR 
Go to: Liquid Propulsion
Go to: Nuclear and Future Flight Propulsion
Go to: Pressure Gain Combustion
Go to: Propellants and Combustion
Go to: Propulsion and Power of Unmanned Aerial Systems
Go to: Propulsion Education
Go to: Solar and Beamed Energy Sail Concepts and Missions

Go to: Solid Rocket Propulsion
Go to: Small Satellites  
Go to: Space Architecture and Habitation
Go to: Space Logistics and Supportability  
Go to: Space Nuclear Power Systems
Go to: Space Solar Power
Go to: Space Systems
Go to: Space Transportation  
Go to: Thermal Management Technology
Go to: AIAA/IEEE Electric Aircraft Technologies Symposium (22-24 August)

Additive Manufacturing for Propulsion Systems

Please direct questions to:
Corinne Sedano, NASA Jet Propulsion Laboratory  

Papers are requested describing recent developments in the use of additive manufacturing for propulsion systems for space vehicles and aircraft (manned and unmanned).   

  • Lessons Learned
  • Manufacturing Technology
  • System Concepts
  • System Level Trade Studies
  • Test Results and Feasibility Under Simulated/Actual Conditions

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Advanced Integrated Intelligent Propulsion Controls

Please direct questions to:
Al Behbahani, U.S. Air Force

The next generation of aircraft will face more challenging demands in both electrical and thermal loads. A critical element to the success of new propulsion technologies that enable reductions in fuel use is the integration of component thermal management technologies and power systems within engine controls and a viable vehicle package. Vehicle operation requires vehicle thermal management systems capable of balancing the needs of multiple vehicle sub-systems that may require heat for operation, require cooling to reject heat, or require operation within specified temperature ranges.

Developing advanced controls and health management (HM) technologies that will help meet these challenges through the concept of Advanced Intelligent Propulsion Systems. The key enabling technologies for an Intelligent Propulsion System are  active control, advanced diagnostics and prognostics integrated with intelligent engine control to enhance operational reliability and component life, and distributed control with smart sensors and actuators in an adaptive fault tolerant architecture. The objective of advanced intelligent engine controls is to develop and validate advanced control system and health prognostics and diagnostics technologies that are critical to enhancing the safety, reliability and operability of aerospace propulsion systems. 

  • Active/Adaptive Control, Centralized/Decentralized Fault Tolerant Tracking Control Systems
  • Advanced Diagnostics/Prognostics Engine Health Management, Engine Health Monitoring
  • Autonomous Propulsion Systems, Intelligent Flight Control, Intelligent Aerospace Systems
  • Communication Bus, Databus, Smart Sensors and Actuators, Flexible/Extensible Smart Components
  • Data Analytics Using Machine Learning, Artificial Neural Network Configurations and Other Artificial Intelligence-Based Models
  • Hierarchical/supervisory Control Algorithms, Logic Controller Designs, Redundancy Issues
  • Intelligent/Robust Sensor Network, Wireless Sensor Networking, Fiber Optic Sensing/Communication
  • Optimal Fuel Use Strategies, Advanced Thermal Management, Integrated Power Systems

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Advanced Mechanical Components

Please direct questions to:
Patrick Dunlap, NASA Glenn Research Center

Papers are requested describing recent developments in: system-level trade studies evaluating competing sealing approaches on the basis of performance metrics, new seal design concepts and sealing approaches showing promise, methods for seal design and predicting seal performance under service conditions, coupled techniques, test results demonstrating concept feasibility under simulated/actual conditions, and  novel test rigs and seal material advancements. These sessions are sponsored by the ASME Propulsion Technical Committee.

  • Advanced Seal Technology
  • Coupled Techniques (Exp. or Analytical) to Study Interaction Between Seal, Cavity, and Main Flows
  • Descriptions of Novel Test Rigs Used to Evaluate Seal Concept Performance
  • Methods for Seal Design and Predicting Seal Performance Under Service Conditions
  • New Seal Design Concepts and Sealing Approaches Showing Promise of Meeting Performance Requirements
  • Seal Material Advancements to Improve Performance or Extend Life
  • System-Level Trade Studies Evaluating Competing Sealing Approaches Based on Performance Metrics
  • Test Results Demonstrating Concept Feasibility Under Simulated/actual Conditions

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Advanced Propulsion Concepts 

Please direct questions to:
John Robinson, Boeing (retired)

Papers are sought in the area of unique propulsion systems for Earth-to-orbit launch systems, space systems, advanced compact systems, nano-propulsion systems, reciprocating systems, and lightweight aircraft engines. In the area of innovative approaches and advance conventional systems, papers are sought that show theoretical, computational, or experimental results; mission analysis; and instrumentation and diagnostic techniques. Papers on in-situ propellants for lunar or Mars missions should address propellant production, theoretical and experimental designs, and evaluations and analysis for current and future applications.  

  • Innovative Approaches and Advanced Conventional Systems
  • In-Situ Propellants for Asteroid, Lunar or Mars Missions
  • Unique Propulsion Systems

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Advanced Vehicle Systems

Please direct questions to:
Frank Chandler, Cal Poly Pomona

Papers are solicited for advanced vehicle system concepts including small satellite launch vehicles,  large launch systems and hypersonic vehicles.  Particular interests in the recent advances in the development of small launch vehicles for CubeSat delivery to orbit, hypersonic vehicle flight experiments, and new launch systems for delivery of commercial and/or National Security Payloads. Papers covering the following are sought: development status, and flight test results for innovative, advancing state-of-art, vehicle systems for atmospheric, trans-atmospheric, and space exploration vehicles (novel spacecraft concepts, flight experiments, etc.) systems.  Papers on critical subsystem technologies that enable new missions are also welcomed, including but not limited to integrated propulsion systems,  space power generation, storage, management & distribution (PMAD), robotic & autonomous systems (sensing, mobility, autonomy, autonomous rendezvous & docking (AR&D), deep space communication & tracking systems, advanced habitat/ life support systems, In-situ resource utilization (ISRU) for propellant manufacturing, abort/crew escape system, and critical vehicle thermal management systems. This session is sponsored by the ASME Propulsion Technical Committee.

  • Abort/Crew Escape Systems and Critical Vehicle Thermal Management Systems
  • Advanced Habitat/Life Support, In-Situ Resource Utilization for Propellant Manufacturing Systems
  • Critical Enabling Subsystem Technologies
  • Deep Space Communication and Tracking Systems
  • Hypersonic Vehicle Flight Experiments
  • Large Launch Vehicle Systems
  • Robotic and Autonomous Systems; Autonomous Rendezvous and Docking (AR&D) Systems
  • Small Satellite Launch Vehicle Systems
  • Space Power Generation, Storage, Management and Distribution
  • Vehicle Systems for Atmospheric, Trans-Atmospheric and Space Exploration

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Aerospace Power Systems

Please direct questions to:
Abbas Salim, Lockheed Martin Corporation (retired)

Papers are sought on all sorts of Space Power Systems discussing study findings, results of practical applications, tests, simulations, short and long term performance, and R&D initiatives. Specific topical areas are listed below. However, authors are encouraged to submit papers on other innovative ideas and topics related to Space Power Systems.                                                                   

  • CubeSat Programs:  Ground Testing and Flight Results From Custom-Made and COTS Systems; Lessons Learned From Mission Failures; and Coping with Special Requirements
  • End of Life Passivation of Spacecraft Electric Power Eneration and Storage Devices
  • LEO/MEO/GEO Spacecraft Power System Design, Fabrication, Testing, in-Orbit Experience and Lessons Learned
  • Lunar and Mars Surface Power Systems
  • New and Unique Power System Technologies for Space Platforms
  • Next Generation High Voltage Electrical Power System Design and Distribution for >50+ KW Space Applications
  • Power Generation, Control and Distribution for Electric Propulsion Including Power Processing Units
  • Power System Designs for Large LEO Spacecraft Constellations Including Maintenance and Refurbishment
  • Spacecraft Power Systems and Flight Experience for Near and Deep Space Missions

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Electric Propulsion

Please direct questions to:
Wensheng Huang, NASA Glenn Research Center

Papers are solicited for sessions on electric propulsion related technologies, systems, components, modeling, and fundamental physics. Of particular interest are papers relating to a range of electric propulsion technologies including, but not limited to: missions utilizing electric propulsion, flight systems, hall thrusters, ion thrusters, power processing units, propellant management systems, gimbals, micropropulsion concepts, electrospray thrusters, magnetoplasmadynamic thrusters, pulsed-plasma thrusters, pulse-inductive thrusters, electrothermal thrusters, and tethers. Papers are also sought on topics regarding innovative and/or advanced electric propulsion technologies, propulsion and plasma diagnostics, and electric propulsion simulations.

  • Advanced Concepts
  • Cathode
  • Cubesat/Smallsat and other Micro-Electric Propulsion
  • Electric Propulsion Flight Programs and Missions
  • Electric Propulsion Spacecraft Integration
  • EP Diagnostics
  • EP Modeling
  • Hall Thruster
  • Ion Thruster
  • Power Processing
  • Propellant Management for Electric Propulsion Applications

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Electricity Delivery and Grid Reliability

Please direct questions to:
Scott Duncan, Georgia Institute of Technology
Ryoichi S Amano, University of Wisconsin-Milwaukee

Technical papers are being sought that address the latest research, developments, and viable new technologies applicable to energy delivery for terrestrial systems, e.g., electric grids, micro grids, district thermal energy systems, ground-based battery charging.  

  • Demand-Side Energy Management Technologies, Including Demand Response
  • Grid Impacts of Techs that Pair Electric & Thermomechanical Energy Production e.g., Cogen and CHP
  • Grid Reliability, Including Fault Current Limiters, Smart Grid Systems, Fault Detection, etc.
  • Transmission and Distribution Technologies, Including Distributed Generation and Power Electronics

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Energetic Components and Systems

Please direct questions to:
Stephanie Sawhill, Systima

Papers are solicited that are related to the development, demonstration, qualification and production of propellant- or explosive-actuated mechanisms and gas generators used in aerospace, military aircraft, and commercial applications. Topics of interest include, but are not limited to, Explosive Theory and Initiation, Cartridge Actuated Devices; Propellant Actuated Devices; Thrusters; Propellant and Explosive Compositions; Ballistic Analysis; Non-Pyrotechnic Mechanisms; Systems Integration; and Studies on Acceptance Criteria and Manufacture. 

  • Design, Testing and Acceptance of Space Mechanisms and Systems
  • Detonation Theory and Initiation
  • Energetic (Explosives, Propellants and Combustible)  Component Heritage
  • Energetic Components used in Military or Commercial Aircraft, and Safety Systems
  • Explosive and Propellant Compositions
  • Explosive- or Propellant- Actuated Mechanisms and Systems
  • Innovation in Failure Investigation and Analysis, and Environment Testing
  • Physics of Interior Ballistics in Explosive, Propellant, Combustible Devices
  • University-Led Advanced Research of New Propellant and Explosive Formulations and Their Application

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Energy Conversion Technology

Please direct questions to:
Ed Lewandowski, NASA Glenn Research Center

Technical papers are requested on research and development in the area of space and terrestrial power system energy conversion. Contributions may address initial concepts, simulation, prototype testing, fabrication, applications of, and novel system integration and analysis. Areas also include performance, modeling, analysis, testing, calibration, and operation of static and dynamic energy conversion devices. 

  • Cryogenic Technologies for High Power Density for Aerospace
  • Dynamic Energy Conversion Devices (Brayton, Rankine, Stirling, etc.)
  • Emerging, Small Scale Energy Conversion Devices - Sensors and Power Systems
  • Magnetohydrodynamic (MHD) Power Conversion
  • Static Energy Conversion Devices (PV, Thermionics, Thermoelectrics, Thermo-PV, etc.)
  • Stirling Engines and Radioisotope Power Systems

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Energy-Efficient and Renewable Energy Technologies

Please direct questions to:
Li Qiao, Purdue University
David Carrington, Los Alamos National Laboratory  
Ryoichi Amano, University of Wisconsin-Milwaukee  
Scott Duncan, Georgia Institute of Technology  

Renewable Energy Technology includes Wind, Solar, Hydro, Biomass, and Geothermal Energy. Energy-Efficient Topic includes supercritical combustion, combined heat and power, energy saving technology, advanced combustion and power-cycles, innovative energy management and controls, nuclear power for aerospace, energy storage, thermal management, advanced materials for power cycles.

  • Energy-Efficient Protocols and Power Management
  • Energy-Efficient Transmission Technologies
  • Experimental Studies in Energy-Efficient Systems
  • Green Energy Issues
  • Green Energy Power Generation Simulation and Modeling
  • Simulation/Modeling for Energy Efficient Solutions
  • Technology Development in Renewable Energy Systems

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Fuel and Power Generation Technology

Please direct questions to:
David Carrington, Los Alamos National Laboratory
Li Qiao, Purdue University
Scott Duncan, Georgia Institute of Technology
Ryoichi Amano, University of Wisconsin-Milwaukee 

Technical papers in simulation, modeling and experiments as related to combustion of fossil fuels to deliver work and power. This topic area includes the combustion process to release chemical energy available in any carbon-based fuel in burners or engines, the processes of direct conversion of energy from engines or turbines,  or indirect conversion to a working fluid and subsequent conversion in turbines or engines. Also of interest is waste heat recovery, fuel type conversion, and combustion product treatments and mitigation. 

  • Applications of Nanotechnology for Fossil-Fuel Power Technologies
  • Combined Heat and Power with Ultra-Low Emission of Pollutants and Particulates
  • Combustion Turbines, Advanced Combustion and Power Cycles
  • Fire, Super-Critical Combustion
  • Fuel and Gas From Shale and Deep-Water Regions
  • Fuels, Alternative Fuels, Coal, Natural Gas, Oil, Gas From Methane Hydrate
  • Gasification, Innovative Energy Management in Smart Cities, Big Data, and Controls
  • Lean Coal and Natural Gas Power Systems, Combustion, Advanced Designs, Micro-Combustors
  • Pollution and Chemical Kinetics, CO2 Use for Fuels and Value Added Products

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    Gas Turbine Engines

    Please direct questions to:
    Andrew Yatsko, Georgia Institute of Technology
    Rebecca Howard, Air Force Research Laboratory

    Papers are solicited in the disciplines of thermodynamics, aerodynamics, aeroelasticity, mechanical design and manufacturing, combustion, heat transfer, anti-icing and controls as related to the science, research, technology development, and testing of gas turbine engines. This includes related components for air vehicles in the subsonic and transonic flight regimes and gas turbine matching  with air vehicles.

    • Application of Metallurgy and/or Manufacturing Techniques (such as CMC and Additive Manufacturing)
    • Cycle Performance Matching With Aircraft Performance
    • Electric Power Generation; "Green"/environmentally Friendly Aviation; Alternative Fuels
    • Engine Controls; Diagnostics/Health-Monitoring/CBM Techniques; Advanced Instrumentation/Sensors
    • Engine Cycles/architectures/Installations; Variable Cycle Engines; Turbo-Electric Propulsion
    • Engine Test Techniques (Component Tests, Data Analysis, the Comparison of Flight and Ground Tests)
    • Engine-Related Heat Transfer, Thermal Management, Cooling, and Secondary Flow Management; Durability
    • Multidisciplinary Design, Analysis/Optimization of Engine Systems and Components
    • Technologies in Higher Efficiency and Lower Noise (such as Geared Turbofans and Auxiliary Systems)
    • Turbomachinery: Computational and Experimental Work on Compressor/Turbine Design and Performance

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      High-Speed Air-Breathing Propulsion

      Please direct questions to:
      Erik L. Axdahl, NASA Langley Research Center

      Technical papers are sought for fundamental research and applied development efforts to advance the state of the art of high speed, air breathing propulsion.  Topics in numerical analysis, theory, ground test, or flight test are desired.  Papers should be relevant to the development, analysis, optimization, or integration of scramjet, ramjet, dual-mode, or pressure gain engines and their components (e.g. inlets, isolators, combustors, injectors, nozzles).  

      • Additive Manufacturing Techniques, Including Thermal-Mechanical Material Characterization
      • Chemical Mechanism or Thermal Models for New Fuels, Including Reduced Models
      • Flowpath or Component Optimization and Performance Prediction
      • Fuel Injection, Mixing, and Flameholding, Including Characterization of Losses or Gains
      • Modeling and Simulation Development, Including Efforts In Model-Based Systems Engineering
      • Novel Combined Cycle Concepts
      • Pulse or Rotating Detonation Engines
      • Thermal Management
      • Turbine- or Rocket-Based Combined Cycle Concepts
      • Uncertainty Quantification and Propagation

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        Hybrid Rockets

        Please direct questions to:
        Shane Coogan, Southwest Research Institute
           
        This topic involves experimental, theoretical, and numerical work in all areas related to design, novel fuel chemistry, enhancement of fuel and oxidizer performance and internal geometry requirements for liquid, solid, and gaseous fueled Hybrid and Bi-Propellant Rocket Systems for stable operation.

        • Business Case, Financials, and Future Investment in Hybrid Propulsion Systems
        • Combustion Dynamics, Mixing Efficiencies, and Fuel/Oxidizer Chemical Kinetics
        • Combustion Stability, Motor Performance, and Related Issues
        • Contemporary Hybrid Rocket Fuel Characterization, Visualization, and Controls
        • Descriptions of Current Programs – Their Objectives and Progress to Date
        • Design and Development of Novel Hybrid Rocket Motor Concepts
        • Design Studies Including Cost and Feasibility Analysis
        • Development and Evaluation of Novel Oxidizer and Fuel Formulations and Combinations
        • Educational STEM Initiatives for Hybrid Propulsion Systems
        • Green Propellants, Contemporary Materials, and Advanced Manufacturing Techniques
        • Historical Accounts of Hybrid Rocket Propulsion
        • Injector Designs and Effect on Engine Performance and Stability
        • Internal Ballistics Modeling Including Predictive Capability
        • Oxidizer Vaporization, Heat Transfer, Species Evolution, and Mixing of Oxidizer and Fuel Species

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          Inlets, Nozzles, and Propulsion Systems Integration

          Please direct questions to:
          Russell Thornock
          Stephanie Hirt, NASA Glenn Research Center 

          INPSI is concerned with the design and analysis of inlets, ducts, and nozzles for flight vehicles operating in flight regimes from subsonic through hypersonic, and the integration with the engine, as well as unducted fans. Included in this are sic design aspects such as icing, particle separation, propulsion system controls, and angle of attack and crosswind performance. Unconventional and innovative propulsion systems have received recent interest due to new vehicle missions, airframe concepts, engine technologies, and fuel economy requirements. More efficient propulsion system designs and technology are being investigated that present challenges for existing and new aircraft designs in terms of integration, performance, and operability. We seek papers exploring the the above topics and trends and in the following areas:

          • Inlet/Exhaust System Integration Design, Performance, and/or Operability
          • Integration of Propulsion and Flight Controls for Urban Air Mobility and Distributed Propulsion
          • Integration of Secondary Power Systems and Impact on Performance
          • Optimization of Propulsion System Design and Integration
          • Propulsion Aerodynamics Workshop
          • Propulsors and Subsystems for Air Breathing Electric Propulsion
          • Smart Materials and Structural Systems in Aerospace Applications
          • Thermal Management Aspects of Propulsion System Performance
          • Unducted Fan Design, Performance or Analysis

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            ITAR

            Please direct questions to:  
            Monica Jacinto, Aerojet Rocketdyne

            In the ongoing effort to improve the impact of AIAA events for members, ITAR sessions will continue to be organized with the intent of expanding the breadth of topics and emphasizing sessions with relevance to Forum 360 events and major elements of the open technical sessions. Submission of groups of presentations representing major accomplishments or status updates of significant system development programs are encouraged.This year, key focus areas are air-breathing, electric, hypersonic, nuclear and rocket, primary and secondary propulsion systems and energetics. Topics aligned with technical committee tutorials or panel sessions planned for 2019 are also encouraged.

            All abstracts must be unrestricted and cleared for public release, though the final papers and presentations will be ITAR restricted. Click  here to make sure you meet the attendance and submission requirement to present in ITAR sessions.

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            Liquid Propulsion

            Please direct questions to:
            BJ Austin, INSPACE, LLC

            Papers are sought from all areas related to liquid rocket propulsion, including component and system level technologies, new concepts and applications, related research and development programs, associated test facilities, and modeling approaches. Topics of interest include, but are not limited to:

            • Combustor Design, Analysis, and Testing Including Igniters, Cooling Methods, and Instability Studies
            • Current and Historical Lessons Learned In Liquid Propulsion Development and Operation
            • Green and Non-Toxic Propellant Studies, Development, Applications, and Associated Technologies
            • Injector Design, Analysis, and Testing Including Atomization and Mixing Studies
            • In-Space Liquid Propulsion System Design, Analysis, Testing, and Operation Including for Cube/Nanosats
            • Launch Vehicle Liquid Propulsion System Design, Analysis, Testing, and Operation
            • Modeling and Simulation of Liquid Propulsion Systems, Components, and Processes
            • Novel Manufacturing Technologies and Advanced Materials for Application to Liquid Propulsion Systems
            • Nozzles Design, Analysis and Testing Including Thrust Vectoring Methods
            • Propellant Feed System Design, Analysis, and Testing
            • Propellant Management and Storage Design, Analysis, and Testing Including Related to In-Orbit Refueling
            • Test Facilities and Advanced Diagnostic Techniques Relevant to Liquid Propulsion
            • Turbomachinery and Electric Pump Design, Analysis, and Testing Including Structural Dynamics and FSI

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            Nuclear and Future Flight Propulsion

            Please direct questions to:
            Jim Cavera, Consultant

            Papers should address approaches for nuclear-powered rocketry and alternative, physics-based propulsion systems. Relevant topics include all aspects of nuclear thermal rocket (NTR) design, testing, and utilization as well as innovative or emerging concepts for fusion-based, antimatter or hybrid space systems. “Future Flight” topics include concepts for both near- and far-term propulsion architectures that require significant advancements in physics and propulsion science. Applications of space-time manipulation, gravity modification, electromagnetic coupling, particle/quantum physics, relativistic assessments or fluidic continua are valid for this area. Future Flight papers should be well-founded in theory and clearly identify a propulsion application. Any performance comparisons must include uncertainty bands.

            • Fusion, Alternative Nuclear, and Antimatter Concepts
            • Future Flight Propulsion Systems
            • Nuclear Electric and Bimodal Concepts
            • Nuclear Thermal Propulsion: Engine Modeling
            • Nuclear Thermal Propulsion: Fuels and Materials
            • Nuclear Thermal Propulsion: Testing and Programmatics

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            Pressure Gain Combustion

            Please direct questions to:
            Greg Meholic, The Aerospace Corporation

            Papers relating to Pressure Gain Combustion (PGC) can be submitted to the following subtopics: Physics Modeling and Exploration papers would focus on analytical and empirical efforts to examine the fundamental aspects of detonation combustion such as wave formation and dynamics, heat loss and transfer mechanisms, propellant mixing and other similar topics. Papers in the Component and Subsystem Development category would describe the analysis, design or test of systems needed to support PGC operation such as propellant delivery, ignition, and cooling. Discussions of specific components such as turbines and nozzles can also be included. Performance, Integration and Applications papers would discuss analytical or empirical investigations of PGC performance sensitivities due to changes in inlet/outlet conditions, operational adjustments, component configuration or influences from downstream hardware. Papers in this category could also describe the integration of PGC systems into terrestrial, atmospheric or space applications as well as novel configurations. Measurement Techniques and Test Facilities papers would describe instrumentation or data processing approaches applicable to unsteady environments that could aid in characterizing thrust, performance or flow field measurements. This topic would also include descriptions of dedicated PGC test facilities or upgrades. 

            • Pressure Gain Combustion Component and Subsystem Development
            • Pressure Gain Combustion Measurement Techniques and Test Facilities
            • Pressure Gain Combustion Performance, Integration and Applications
            • Pressure Gain Combustion Physics Modeling and Exploration

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            Propellants and Combustion

            Please direct questions to:
            Venke Sankaran, Air Force Research Laboratory

            Papers are sought describing experimental, analytical, and numerical work in all areas related to combustion of liquid, solid, and gaseous fuels in rocket, air-breathing, and other propulsion and power systems. Topics include but are not limited to:

            • Combustion Diagnostics
            • Combustion Dynamics and Instabilities
            • Combustion Performance of Additively Manufactured (AM) Components and Fuels
            • Data Analysis and Data Assimilation Techniques
            • Development of New Fuels, Propellants, and Energetic Materials
            • Formulation and Decomposition of Monopropellants and Endothermic Fuels
            • Ignition
            • Kinetics of Solid-, Liquid-, and Gas-Phase Combustion
            • Micro-Scale Combustion and Other New Combustion Concepts
            • Physics-Based/High-Fidelity Models
            • Reduced-Order and Multi-Fidelity Models
            • Spray Behavior and Combustion

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            Propulsion and Power of Unmanned Aerial Systems

            Please direct questions to:
            Lea-Der Chen, Texas A&M University

            Technical papers are sought on propulsion and power of autonomous systems including unmanned aircraft systems and autonomous ground vehicles. Topics of interest include (a) energy harvesting and management; (b) conventional and alternative power systems: combustion engines, fuel cell, solar panel, and battery; (c) dynamics and control; (d) communication and connectivity; and (e) applications of autonomous vehicles.  Papers of exploratory investigations, modeling and simulation, payload implementation, and sensor integration are also welcome. 

            • Alternative Power Systems: Fuel Cell, Solar Panel, Battery
            • Applications of Autonomous Systems including Unmanned Aerial Systems, Air Mobility Applications
            • Combustion Engines: Gas Turbine, Internal Combustion, and Pulse Detonation
            • Dynamics and Control: Aerodynamics, Flight Control, Payload Implementation, Sensor Integration
            • Energy and Power Management of Autonomous Systems
            • Energy Harvesting
            • Hybrid Power Systems
            • Modeling and Simulation of Power Sub-Systems
            • Operations and Control of Multi-Agents/Multi-Model Systems

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            Propulsion Education

            Please direct questions to:
            Robert A. Frederick, Jr., University of Alabama at Huntsville

            Papers can cover STEM outreach programs, university curriculum, student projects and research, university research programs and history, new university laboratory capabilities, new university curricula, international partnerships, student launch projects, safety aspect of university projects, technology control plans for university research, and propulsion literature reviews. Topics of interest include the following:

            • STEM Outreach: K-12 Outreach, Minority Outreach, and Community Outreach Programs
            • Student Projects: Student Launch Competitions, Student Design Projects, Student Research Projects
            • University Programs: Overview of Propulsion Curricula, Description of Classes, Laboratories, or Academic Programs.
            • University Propulsion Safety: Considerations for University Projects and Research
            • University Research: Strategies, Research Center Overviews, Laboratory Capabilities, University Program History

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            Solar and Beamed Energy Sail Concepts and Missions

            Please direct questions to:
            Jim Cavera, Obligatory LLC
            John Robinson, The Boeing Company (retired)
            Harold White, NASA Johnson Space Center

            Papers are solicited for sessions on solar and beamed energy sail concepts and approaches. Of particular interest (but not limited to) are papers detailing materials and manufacturing techniques to be used in solar sail construction, solar sail stow and deploy approaches, spacecraft maneuvering, dust impact quantification and mitigation, ablation augmentation of thrust magnitude, charged sails techniques, beamed sail approaches including technical/economical details on ground/space installations to serve as beam source for beamed sail approaches. Papers are also sought that detail mission approaches for the technologies ranging from demonstration missions, earth centric and inner solar system missions (e.g. inside Jupiter orbit), outer solar system and deep space missions, interstellar precursors, and interstellar missions.

            • Beamed Energy Solutions
            • Novel Sail Approaches
            • Sail Control
            • Sail Deployment
            • Sail Materials
            • Sail Missions

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            Solid Rocket Propulsion

            Please direct questions to:
            Wesley J. Ryan, NASA Kennedy Space Center
            Eldon Triggs, Auburn University

            Papers are solicited that relate to all aspects of solid rocket propulsion systems, including component and system-level design, material development/selection, manufacturing, testing, ballistic prediction methodologies, performance evaluation, and state-of-the art technology advancements.  Additional areas of interest include overviews of historical solid propulsion systems, lessons learned from development, testing and flight experience, and current status of upcoming solid rocket motor systems/programs.  Discussions focused on STEM initiatives, university capabilities, and shifting or emerging trends in government and industry are also welcome.

            • Acoustic Characterization and Combustion Stability
            • Case, Nozzle, and Ignition System Design Innovations
            • Controllable Solid Propulsion/Thrust Management Techniques
            • Current Solid Propulsion System Development Efforts and Program Status
            • Future Solid Propulsion Technologies
            • Historic Solid Propulsion Systems and Lessons Learned
            • Modeling and Simulation Advancements
            • Motor Design and System Optimization
            • Propellant Chemistry, Synthesis, and Characterization
            • Propellant Geometry and Ballistics
            • University-Based Solid Rocket Motor Programs

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            Small Satellites

            Please direct questions to:
            Jeremy Straub, North Dakota University

            This track covers all aspects of small satellites and their missions.  Papers are particularly encouraged that have a focus on small satellite propulsion topics; however, papers on other areas of small satellites are also welcomed. Topics include small satellite design, development and systems engineering, mission operations and spacecraft subsystems. We are also interested in papers discussing launch capabilities for small spacecraft and policy considerations related to small spacecraft and their use. Papers are also welcome that discuss success factors for small spacecraft missions, as are those regarding education related to small spacecraft development or the use of small spacecraft in other educational activities (formal or informal).Acoustic Characterization and Combustion Stability

            • Board/Chip SATS
            • Control (Including Autonomy) for Small Spacecraft
            • CubeSats
            • Dedicated Launch Capabilities for Small Satellites
            • Educational Activities (Informal and Formal) Related to or Using Small Spacecraft
            • ESPA-Class Spacecraft
            • Other Small Satellites
            • Rideshare Capabilities
            • Small Satellites
            • Small Spacecraft Communications
            • Small Spacecraft Missions (Including Flown and Planned)
            • Subsystems for Small Spacecraft
            • Use of Small Spacecraft Beyond Earth Orbit
            • Use of Small Spacecraft in Clusters or Federated Systems

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            Space Architecture and Habitation

            Please direct questions to: 
            Matthew Simon, NASA Langley Research Center 

            We face into a future rich with inspiring and historic visions: for human exploration of space; for tourism and settlement; and for development of space resources. Mission concepts, system architecture, and habitation technologies lay at the heart of all these visions. The Space Architecture and Habitation track, sponsored by AIAA's Space Architecture Technical Committees, welcomes detailed and interdisciplinary papers about all aspects of the human adventure in space and reports on on-going and recently concluded professional and student projects. Accepted papers will be organized by the TCs into thematic sessions in areas such as:

            • Colonies and Settlements
            • Human Factors at All Scales
            • Space Architecture Aspects of Exploration Mission Concepts
            • Space Architecture: Habitats, Infrastructure, and Construction
            • Space Flight Analogs and Simulators
            • System-Level Integration of Advanced Technologies

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            Space Logistics and Supportability

            Please direct questions to: 
            Kandyce Goodliff, NASA Langley Research Center

            Space logistics is the theory and practice of driving space system design for operability, and of managing the flow of material, services, and information needed throughout a space system lifecycle. It includes management of the logistics supply chain from Earth and on to destinations throughout the solar system. Supportability considers strategies to minimize both logistics requirements and operational costs of human and robotic operations. Supportability strategies include processes and technologies to minimize maintenance complexity, exploit in-situ resources, scavenge and reuse flight hardware, and recycle consumables. Representative areas include the servicing and sustainment of the International Space Station and of lunar and planetary outposts, the optimization of logistics launch vehicles for responsiveness and serviceability, and modeling of the supply chain in space for human and robotic mission campaigns.

            • Advanced Destination Logistics: Outpost Management, in-Situ Resource Logistics, EVA Logistics
            • Advanced Supportability Concepts: in-Situ Repair & Fabrication, Recycling, Scavenging & Reuse
            • Automated Spaceflight Supply Chain Asset Tracking and Monitoring
            • Commercial Space Logistics Opportunities
            • Infrastructures: Fuel Depots, Refueling in Space, Planetary/asteroid Resource Infrastructures
            • In-Space Spacecraft and Satellite Servicing
            • Logistics Approaches: Space Operations Affordability, Commonality, Integrated Logistics Concepts
            • Space Logistics Campaign Planning: Methods, Modeling, Simulation, and Cost Analysis Tools

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              Space Nuclear Power Systems

              Please direct questions to:
              Greg Semrau, Moog, Inc.

              This topic focuses on complete nuclear power system beyond components. This takes into account the balance of plant, system architectures, unique features, usage of radiation tolerant components for new system level techniques and concerns with the supply of Plutonium-238. Of interest would be recent developments in the realm of radioisotope power systems (generators, reformers, power electronics, thermal management), these developments could be increased efficiency, reliability or environmental survivability.

              • Nuclear Thermal Propulsion and/or Nuclear Electric Propulsion
              • Power Systems for Planetary Power Production (Mars or Other Planets)
              • Power Systems for Satellite/Deep Space Power Production
              • Space Probes based on Nuclear Power or Radioisotope Systems
              • Space Transportation Topics using Nuclear Power
              • The Balance of Plant for Nuclear Power or Radioisotope Systems

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              Space Transportation

              Please direct questions to:
              Brian Pomeroy, Sierra Nevada Corporation 

              The commercial, military, scientific, and human exploration of space depends upon highly reliable access at reasonable costs. Commercial companies have offered the promise of low-cost space access, and some are currently developing, testing, and operating their systems. NASA has begun operation of low-cost, reliable commercial cargo delivery, and is developing crew delivery, to the International Space Station (ISS). The NASA Space Launch System (SLS) will provide the Orion crewed spacecraft a capability to reach deep space destinations. Launch capabilities are also emerging on several fronts to transport the increasing number of small satellite payloads to orbit. 

              • Emerging Launch System Designs, Concepts, and Developments
              • In-Space Transportation Systems and Architectures, Including Propellant Depots
              • Launch Vehicles and Systems (Including Suborbital)
              • Lessons Learned From Previous Programs and Design Studies
              • Operations of Spaceports and Ranges
              • Propulsion Enabling Novel Space Transportation Architectures
              • RLV Development, Programmatic (Including Economics), and Industry-Related Strategies
              • Space Transportation Analytical Tools, Materials, and Technologies
              • Space Transportation for Space Tourism
              • Space Transportation Technology Design, and Integration Challenges

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                Space Solar Power

                Please direct questions to:
                Giang Lam, Lockheed Martin Corporation

                This topic is about the applications of solar power as the primary power generation source for Electrical Power Systems on space satellite designs. Papers related to solar array designs that have flown or baselined to be flown in earth orbit (LEO, MEO or GEO) and on interplanetary missions will be relevant. Additional topics include emerging photovoltaic technologies such as higher efficiency photovoltaic applications, higher power (>20 kW) flexible solar array designs, solar concentrators, and usage in conjunction with Electric Propulsion.

                • Building New Technologies through NASA's Solar Electric Power (SEP) Program
                • Large Solar Array Design (>25kW) and Flight Performance
                • Solar Array Concentrator Mission Design
                • Solar Array Design for High Current and High Voltage EPS
                • Solar Array Design for Interplanetary Missions
                • Solar Array Design for Smallsats and CubeSats
                • Space Exploration with Solar Arrays and Electric Propulsion Systems

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                Space Systems

                Please direct questions to: 
                Patrick Chai, NASA Langley Research Center
                John Bloomer, Raytheon Space & Airborne Systems

                The Space Systems and Sensors track seeks to present important findings from recent work on emerging space systems, space science, and sensor technologies. In particular, papers are sought that address technical, operational, and economic feasibility of current and future space systems that address the full range of civil, military, educational, and international applications. Papers by students are especially encouraged.

                • Additive Manufacturing of Space Systems
                • Advanced Space Propulsion and Energy Systems
                • Education Outreach in Space Systems, Space Science, and Space Technologies
                • Emerging Technologies and Applications for Global Benefit
                • Enabling Technologies for Distributed or Fractionated Space
                • In-Space Assembly and In-Space Servicing
                • Onboard Processing and Intelligent Sensing
                • Remote Sensing for Climate and Weather
                • Space and Planetary Science Mission Science and Technologies
                • Space Policy
                • Space System Architectures and Concepts of Operation

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                  Thermal Management Technology

                  Please direct questions to:
                  Michael Choi, NASA Goddard Space Flight Center

                  Papers discussing study results, operational performance, results of practical applications, tests, simulations, and R&D initiatives of thermal management technology for aerospace and terrestrial applications are encouraged.

                  • Heat Transfer & Transport, Including Two-Phase, Phase Change, Advanced Materials & Spray Cooling
                  • Nanotechnology for Thermal Management, Including Nanoscale Particles, Channels, Wires  & Films
                  • Thermal Energy Storage, Including Advanced Materials, Phase Change Materials, Applications & Issues
                  • Thermal Modeling, Simulation & Analysis, Including Analytical Techniques & Software
                  • Thermal System Applications & Unique Environment, Including Spacecraft, Aircraft and Propulsion
                  • Thermal Systems & Components, Including Electronics Cooling, Cryogenic Systems & Gap Fillers
                  • Thermal Testing on Components, Subsystems and Systems in Vacuum or Ambient Pressure

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                  AIAA/IEEE Electric Aircraft Technologies Symposium (22-24 August)

                  Please direct questions to:
                  Phil Ansell, University of Illinois at Urbana-Champaign

                  The aerospace industry has set ambitious goals for the next three generations of commercial transport aircraft to accommodate rapid growth in emerging markets and ensure sustainability of air travel. One approach being explored to meet these targets is non-traditional aircraft propulsion using electric, turboelectric or hybrid-electric powertrains. Recent events by the IEEE and AIAA have identified the need to bring together electrical engineers and aerospace experts as the industry looks to more electric propulsion technologies for future aircraft. These events include the 2018 EATS, which featured four keynote addresses, an active panel session, 57 technical presentations, and over 170 attendees. 

                  This two and a half-day symposium will focus on electric aircraft technology across three general areas: (1) electric-power enabled aircraft configurations and system requirements, (2) enabling technologies for electric aircraft propulsion, and (3) electric aircraft system integration and controls. Abstracts with a minimum length of 1200 words are encouraged. Successful submissions must also include sufficient detail to demonstrate the purpose of the paper, the technical foundation for the topics to be discussed, any preliminary results to date, and the expected results of the final paper, including key figures, equations, tables, and references, as appropriate. Papers are solicited in all relevant areas including, but not limited to, those listed below.  For more detailed information about each topic please see Additional Details.

                  • Topic Area 1: Aircraft Configurations & Systems Requirements
                  • Topic Area 2: Enabling Technologies and Components
                  • Topic Area 3: System Integration and Controls

                  All are welcome at the Electric Aircraft Technology Symposium, however, please note this event will be co-located with the AIAA Propulsion and Energy Forum and will require a separate registration fee for participants and attendees.
                   
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                  Student Paper Competitions

                  The following Student Paper Competitions are being held in conjunction with the forum:

                  Aerospace Power Student Paper Competition

                  Please direct questions to: 
                  Ann Delleur, NASA Glenn Research Center

                  Undergraduate and graduate students (Master’s level and PhD level) are invited to submit papers for consideration in the Aerospace Power Section Student Paper Competition. Papers should report on original work conducted by the student in collaboration with faculty advisor(s), mentors, and/or industry/government mentors. The student submitting a paper for consideration must be the primary author.

                  Entries to the Aerospace Power Section Student Paper Competition must undergo the regular abstract review process, and if accepted, will be included in the regular technical sessions with other papers in their topic area and be archived as AIAA conference papers. When submitting an abstract for the Aerospace Power Student Paper Competition, authors must choose the “Student Paper Competition” Presentation Type at step 2 of abstract submission, and then select one of the following topics:

                  • Aerospace Power Systems
                  • Energy Conversion Technology
                  • Space Solar Power
                  • Space Nuclear Power Systems

                  The manuscript submission deadline for the Aerospace Power Section Student Paper Competition is the same as the submission deadline for the 2019 AIAA Propulsion & Energy Forum.  All entries to the Student Paper Competition must be received by this date to be considered in the competition. The submissions will be judged based on the paper ONLY. Criteria for judging the paper include 1) originality of the work; 2) scientific integrity, 3) relevance to the field of Aerospace Power; 4) significance technical quality and completeness of the work; and 5) written clarity and style consistent with AIAA paper guidelines.

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                  Dates to Remember

                  • Abstract Deadline: 31 Jan 2019
                  • Manuscript Deadline: 15 Jul 2019

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