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Hypersonic Propulsion at Pratt and Whitney: OverviewPratt & Whitney (P&W) is developing the technology for hypersonic components and engines. A supersonic combustion ramjet (scramjet) database was developed during the National Aero Space Plane (NASP) program using hydrogen fueled propulsion systems for space access vehicles and serves as a point of departure for the current emphasis on hydrocarbon scramjets. The Air Force Hypersonic Technology (HyTech) Office has put programs in place to develop the technologies necessary to demonstrate the operability, performance and structural durability of a liquid hydrocarbon fueled scramjet system that operates from Mach 4 to 8. Fuel-cooled superalloys and lightweight structures are being developed to improve thermal protection and durability and to reduce propulsion system weight. The application of scramjet engine technology as part of combined cycle propulsion systems is also being pursued under NASA and U.S. Air Force sponsorship. The combination of scramjet power and solid rocket booster acceleration is applicable to hypersonic cruise missiles. Scramjets that use gas turbines for low speed acceleration and scramjets using rocket power for low speed acceleration are being studied for application to reusable launch systems and hypersonic cruise vehicles. P&W's recent activities and future plans for hypersonic propulsion will be described.
Document ID
20020092084
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kazmar, Richard R.
(Pratt and Whitney Space Propulsion Weslt Palm Beach, FL United States)
Date Acquired
September 7, 2013
Publication Date
September 29, 2002
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: 11th AIAA/AAAF International Conference on Space Planes and Hypersonic Systems and Technologies
Location: Orleans
Country: France
Start Date: September 29, 2002
End Date: October 4, 2002
Sponsors: American Inst. of Aeronautics and Astronautics, Association Aeronautique et Astronautique de France
Funding Number(s)
CONTRACT_GRANT: NAS8-02001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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