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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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Contents
Introduction ............................................................................................................v
Propulsion Perspective ........................................................................................... 1
Hypersonic Configuration Concepts ........................................................................ 2
Thermodynamics and Materials ............................................................................ 16
The Qu Tube ......................................................................................................... 23
Rocket Propulsion ................................................................................................ 25
Up-and-Down Operations ..................................................................................... 30
Launch Options .................................................................................................... 33
Atmospheric Variations ........................................................................................ 35
Conclusion ............................................................................................................ 37
Appendix A: Historical Perspective ....................................................................... 43
Appendix B: Aeropropulsion Integrated Vehicle ................................................... 46
Appendix C: TAV Operational Costs ...................................................................... 47
Appendix D: Landing Ellipses for Hypersonic Gliders ............................................ 48
Figures
Figure 1. Hardware Flow ........................................................................................ vi
Figure 2. Impact of Air-Breathing Rocket ................................................................ 1
Figure 3. HSVS Hypersonic Cruise Aircraft Showing True Skin Temperature ........... 3
Figure 4. Hypersonic Rocket-Powered Glider Hypersonic Air-Breathing Cruiser ...... 4
Figure 5. Delta-Lifting Body Designs ....................................................................... 5
Figure 6. Martin Marietta X-24 A & B Research Gliders ............................................ 7
Figure 7. Detailed Design Analyses Show the Weight Trends are as Much a
Function of Configuration Family as Lift-to-Drag Ratio ............................ 9
Figure 8. High-Performance Hypersonic Glide Aircraft .......................................... 10
Figure 9. NASA Langley Wing-Body Configuration WB-004 with Critical Areas for
Wing Bodies Identified ........................................................................... 11
Figure 10. FDL-7C/D and FDL-7MC Lifting-Body Configuration .............................. 12
Figure 11. FDL-7C/D with a DuPont Retractable Inward-Turning Inlet. ................ 12
Figure 12. Comparison of FDL-7C/D and Model 176 .............................................. 13
Figure 13. Sufficient Cross Range (L/D) Means There is No Waiting to Return ..... 14
Figure 14. Hypersonic Glider Characteristics ......................................................... 15
Figure 15. Both Delta Planform Lifting Body (Dynasoar) and Model 176 Offer
Superior Landing Performance ............................................................. 16
Figure 16. McDonnell Aircraft Company Roll-Bonded Titanium Structure .............. 17
iii
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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.