NASA's Dual-Fuel Airbreathing Hypersonic Vehicle StudyA Mach 10 cruise vehicle provides a quick response, global reach capability with high survivability. For operations from CONUS, mission radii on the order of 8,000 nmi are sufficient. For missions which return to CONUS, a dual-fueled vehicle is superior, due to its capability to in-flight refuel. However, for one-way mission, an all-hydrogen vehicle is preferable because of its higher specific impulse.
Document ID
20040110965
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Hunt, James L. (NASA Langley Research Center Hampton, VA, United States)
Eiswirth, Edward A. (McDonnell-Douglas Aerospace Saint Louis, MO, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1996
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 96-4591Report Number: AIAA Paper 96-4591