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Defense Intelligence Reference Document Space Access Where We ve Been And Where We Could Go

Defense Intelligence Agency · 56 pages · text from the file's own layer

This Defense Intelligence Reference Document, prepared by the Defense Intelligence Agency and dated 8 March 2010, was produced under the Advanced Aerospace Weapon System Applications (AAWSA) Program. It gives a historical and technical review of how to reach space and return. It covers hypersonic gliders, air-breathing and rocket propulsion, thermodynamics and materials, and launch options. It argues that reliable, schedulable access to low Earth orbit is mainly a hardware and propulsion problem rather than a technology one.

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Rocket Powered
Hypersonic Glider
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' -~"-,
·-----.____ ·-----~~
Combined Cycle
Airbreather Powered
•· Hypersonic Cruiser
Figure 4. Hypersonic Rocket-Powered Glider and Hypersonic Air-Breathing Cruiser
The second configuration is for air-breathing propulsion systems operating at between
mach 6 and mach 14 that require a propulsion-configured vehicle, where the underside
of the vehicle is an integral part of the propulsion system (forming most of the air-
capturing inlet). This is typified by the lower-right vehicle in Figure 4. The thermally
integrated, air-breathing, combined-cycle configuration concept is derived from the
McDonnell Douglas (St. Louis) Advanced Design organization. The vehicle concept
initially conceived in the late 1950s and early 1960s was an air-breathing propulsion-
configured vehicle accelerated by a main rocket in the aft end of the body, as shown in
Figure 3. The vehicle's underside is the propulsion system; the engine is in the engine
module.
Both basic shapes are functions of tau-that is, for a given planform area, the cross-
sectional distribution is determined by the volume required. Tau was reported in
D. KUchemann's book on supersonic aerodynamics6 as:
( 1)
The only configuration discussed in the book in any detail is the rocket-powered
hypersonic glider. The hypersonic glider has greater near-term potential to become an
operational system, considering the failure of the National Aerospace Plane (NASP) to
reach a functional hardware stage.
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Report, from the dia collection. The PDF is mirrored here; the original link is above. 56 pages are in the text index: search them above, or from the library's search.