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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.

  • p. 2 …FY 2009 Advanced Aerospace uestions pertaining to AAWSA Program Bldg 6000, Washington, under the Defense Intelligence…
  • p. 5 …Among the many advances in space access that will be possible in the future,' the key…
  • p. 10 UNCLASSIFIED/,Sf81il 8ffll!ltllt ~!II!! SHLY McDonnell Aircraft Advanced Design Dept. 1958 to 1967 Mr. H…
  • p. 11 …Louis) Advanced Design organization. The vehicle concept initially conceived in the late 1950s and early 1960s…
  • p. 23 …The photo in Figure 16 is from a Society of Automotive Engineers book titled Advanced Engine…
  • p. 30 …to advance beyond a demonstration tube ended in frustration. Any attempt to open the tube results…
  • p. 32 …Propulsion The photo in Figure 27 is from the Society of Automotive Engineers book, Advanced Engine…
  • p. 38 …These solution areas represent the entire propulsion spectrum, from all-rocket (far right) to advanced air…
  • p. 39 …the launcher can return with payload and fuel residuals onboard), use legacy correlations from McDonnell Advanced…
  • p. 45 …why have we advanced so little (as illustrated in Figure 43)? Like the pioneers' Conestoga wagons…
  • p. 47 …to advance beyond a solitary orbital station with limited capabilities. Figure 44 identifies the elements necessary…
  • p. 56 …6 KOchemann, D., "The Aerodynamic Design of Aircraft - A Detailed Introduction to the Current Aerodynamic Knowledge…
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The Russian design bureaus are to thank for arriving at a concept that eliminated the
noisy and hazardous air-breather takeoff and for increasing the operational flexibility of
the British HOTOL concept. Glebe Lozino-Lozinski had a concept for a spacecraft with a
?-metric-ton payload carried atop an Antonov An-225, with a second An-225 carrying
the liquid hydrogen and launch facilities and staff. 3 The An-225 was in fact a mobile
launch facility; it could literally launch a satellite for any facility that could
accommodate a B-747 or an MDC-11. With Rolls Royce or General Electric engines, the
An-225 becomes a more easily maintained vehicle with better altitude performance.
The An-225's empennage is modified from the An-124's single vertical and horizontal
empennage to an 'H' configuration. This permits the powered hypersonic glider to
easily lift off the top of the vehicle, as the MBB Sanger wind tunnel test demonstrated.
Most commercial transport aircraft larger than ERJ 170 are potential mobile launch
platforms for space tourism, point-to-point cargo, or orbital facilities support. Most of
the commercial passenger equipment can be removed, with just enough equipment
remaining for a launch crew. The fuselage is strengthened and fitted with external
mountings for the hypersonic glider. The landing gear need not be modified, as the
same maximum weight as the commercial transport will be maintained. The flight
control system would be adapted to automatically maintain the correct launch
trajectory until separation. A second modified transport would be modified to carry the
liquid hydrogen and liquid air to fuel the hypersonic vehicle, along with maintenance
and support crew. The intent is to use the automatic launch checkout the author
witnessed at Baikanour in 1988, wherein a Soyuz that arrived on its train carrier at
0500 hours launched carrying a Progress capsule at 1715 hours the same day. That
should make a local launch possible within hours of arriving at the specified airport
launch departure site. These two elements can provide a commercial space launch
facility that requires no special or dedicated operational base.
Hypersonic Configuration Concepts
The configuration and the propulsion system are linked through aerothermopropulsion
integration. This approach is not new, as a wide spectrum of configurations and
concepts existed in the 1960s. One such McDonnell Aircraft Company concept is shown
in Figure 3. This potential operational mach 12 cruise vehicle was developed for the
U.S. government as a strike reconnaissance vehicle taking off from a U.S. Air Force
base. The concept was to provide on-demand reconnaissance in force operations.
However, as was the case with all such efforts in the 1960s, none of the aircraft derived
from the "flight-to-space" efforts reached a hardware stage. Individuals working on
these projects were convinced that the industrial capability existed to design and
fabricate these vehicles, and that such vehicles were technically feasible. The concepts
varied widely among different nations, but all had as their goal a transportation system
to space that had commercial potential. This discussion is provided to discriminate
between rocket-powered hypersonic gliders and hypersonic cruisers with an air-
breathing propulsion system.
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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.