B. Aerospace Projects Office
The Aerospace Projects Office (APO), working in close partnership with Air Force
Research Laboratory (AFRL) and the National Aeronautics and Space Administration
(NASA), develops and demonstrates technologies which enable Next Generation
Responsive Strike (Next RS) air platforms. APO envisions reusable hypersonic aircraft
attributes providing future multi-mission strike/ISR capabilities against targets protected
by advanced air defense systems. APO is seeking innovative technologies that close the
gap between the state-of-the- art in reusable hypersonics and the level of technical
maturity required to initiate a NextRS Y-Plane design and development program later this
decade.
APO Relevant Technology Area:
APO recognizes that a full suite of aircraft and mission systems technologies are needed
to eventually field a NextRS weapon system. APO’s focus is strictly on aircraft
technology development and demonstrations that reduce risk in specific technical areas to
enable future design of reusable hypersonic aircraft. These aircraft technologies will be
compatible with the hypersonic environment, modern avionics power/thermal needs and
aircraft-like life cycles and time scales. Areas of interest include:
1. Structures and Materials – technologies for high temperature metallic materials and
structural concepts that allow design of thermally driven, weight-efficient airframes.
2. High Speed Weapon Separation – technologies that allow weapons, weapon bays
and ejection systems to accommodate hypersonic separation from aircraft and flyout
to the target.
3. Dual mode propulsion – technologies that allow continuous powered operation of a
Turbine Based Combined Cycle (TBCC) propulsion system over the entire flight
envelope.
4. Power Generation – technologies that allow power generation sufficient to support a
modern avionics and sensor suite during all periods of flight.
5. Thermal Management Systems – technologies that allow integrated solutions to
managing the thermal environment of the aircraft and propulsion system.
6. High Mach Turbine Engine – technologies that allow efficient TBCC operations
through ascending and descending mode transition without the need for water
injection.