Electric Propulsion Research at AFRL.


Book Description

These viewgraphs contain the following topics: Air Force electric propulsion research emphasis, micro-PPT technical approach, hall thrusters, high performance Hall system overview, risk reduction testing, technology transition, colloid thrusters, modelling and simulation of propulsion/spacecraft interaction, ground measurement needed for thruster emissions, spacecraft effects and basic physics, Hall thruster source modeling, and thruster interaction modeling and simulation.




The USAF Electric Propulsion Research Program


Book Description

All overview of current electric propulsion research and development efforts within the United States Air Force is presented. The Air Force supports electric propulsion primarily through the Air Force Office of Scientific Research (AFOSR), the Air Force Research Laboratory (AFRL) and the AFOSR European Office of Aerospace Research and Development (EOARD). Overall direction for the programs comes from Air Force Space Command (AFSPC), with AFRL mission analysis used to define specific technological advances needed to meet AFSPC mission priorities. AFOSR fluids basic research in electric propulsion throughout the country in both academia and industry. The AFRL Propulsion Directorate conducts electric propulsion efforts in basic research engineering development, and space flight experiments. EOARD supports research at foreign laboratories that feeds directly into AFOSR and AFRL research programs. Current research efforts fall into 3 main categories defined loosely by the thruster power level. All three agencies are conducting research at the low-power regime (P 200W), in support of emerging USAF microsatellite missions. Efforts in the mid-power range (500W to 5kW) is being shifted from research and development to thruster/spacecraft integration issues. The high power regime (P 30kW) is realizing increased emphasis.




Overview of the USAF Electric Propulsion Program


Book Description

An overview of current electric propulsion research and development efforts within the United States Air Force is presented. The Air Force supports electric propulsion primarily through the Air Force Office of Scientific Research (AFOSR), the Air Force Research Laboratory (AFRL) and the AFOSR European Office of Aerospace Research and Development (EOARD). Overall direction for the programs comes from Air Force Space Command (AFSPC), with AFRL mission analysis used to define specific technological advances needed to meet AFSPC priorities. AFOSR funds basic research in electric propulsion throughout the country in both academia and industry. The AFRL Propulsion Directorate conducts electric propulsion efforts in basic research, engineering development, and space flight experiments. EOARD supports research at foreign laboratories that feeds directly into AFSR and AFRL research programs. Current research efforts fall into 3 main categories defined loosely by the thruster power level. All three agencies are conducting research at the low-power regime (P 200 W), in support of emerging USAF microsatellite missions. Efforts in the mid-power range (500 W to 5 kW) are being shifted from research and development to thruster/spacecraft integration issues. The high power regime (P 30 kW) is realizing increased emphasis.




The USAF Electronic Propulsion Research Program


Book Description

All overview of current electric propulsion research and development efforts within the United States Air Force is presented. The Air Force supports electric propulsion primarily through the Air Force Office of Scientific Research (AFOSR), the Air Force Research Laboratory (AFRL) and the AFOSR European Office of Aerospace Research and Development (BOARD). Overall direction for the programs comes from Air Force Space Command (AFSPC), with AFRL mission analysis used to define specific technological advances needed to meet AFSPC mission priorities. AFOSR funds basic research in electric propulsion throughout the country in both academia and industry. The AFRL Propulsion Directorate conducts electric propulsion efforts in basic research, engineering development, and space flight experiments. BOARD supports research at foreign laboratories that feeds directly into AFOSR and AFRL research programs. Current research efforts fall into 3 main categories defined loosely by the thruster power level. All three agencies are conducting research at the low-power regime (P 200 W), in support of emerging USAF microsatellite missions. Efforts in the mid-power range (500 W to 5 kW) is being shifted from research and development to thruster/spacecraft integration issues. The high power regime (P 30 kW) is realizing increased emphasis.




The USAF Electric Propulsion Research Program


Book Description

To provide enhanced satellite maneuvering capability at reduced cost, the United States Air Force (USAF) has developed a coordinated research program within the Air Force Office of Scientific Research (AFOSR), the Air Force Research Laboratory (AFRL), and the AFOSR European Office of Aerospace Research and Development (EOARD). Research direction for these efforts comes primarily from Air Force Space Command (AFSPC) in the form of a Strategic Master Plan (SMP). The SMP provides a 25-year AF plan, detailed in terms of near-term (2000-2007), mid-term (2008-2013), and far- term (2014-2025) development priorities. AFRL and AFOSR perform the mission analysis required to determine the optimal propulsion system for the AFSPC missions, and then develops research programs to develop the 4 technology needed to achieve these missions. EOARD interacts with AFRL and AFOSR to develop research at European laboratories that will directly feed into the AFOSR and AFRL research programs. Near-term missions are generally served through commercial contracts at the System Program Office (SPO) level.







1987 Status Report


Book Description




A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs


Book Description

Rocket and air-breathing propulsion systems are the foundation on which planning for future aerospace systems rests. A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs assesses the existing technical base in these areas and examines the future Air Force capabilities the base will be expected to support. This report also defines gaps and recommends where future warfighter capabilities not yet fully defined could be met by current science and technology development plans.




Air Force Research Laboratory High Power Electric Propulsion Technology Development


Book Description

Space solar power generation systems have a significant impact on Electric Propulsion (EP) technology development. Recent advances in solar cell, deployment, and concentrator hardware have led to significant decreases in component mass, reducing system specific power. Combined with maneuvering requirements for Air Force and DoD missions of interest, propulsive requirements emerge that provide direction for technology investments. Projections for near- to mid-term propulsion capabilities are presented indicating the need for thrusters capable of processing larger amounts of power (100 - 200 kW), operating at relatively moderate specific impulse (2000 - 5000 s) and high efficiency (> 60%), and having low mass (