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Multi-layer stitched blanket insulation 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/58
출원번호 US-0418603 (1989-10-10)
발명자 / 주소
  • Porter John W. (Poway CA) White Neal C. (San Diego CA) Holdridge Jeffrey D. (San Diego CA)
출원인 / 주소
  • General Dynamics Corporation, Space Systems Division (San Diego CA 02)
인용정보 피인용 횟수 : 37  인용 특허 : 0

초록

A multi-layer blanket insulation adapted of use in an aerobrake intended to assist in the return of a space vehicle from a higher earth orbit to a low earth orbit for recovery and possible reuse. Between two face sheets of a cloth material highly resistant to elevated temperatures are interposed a l

대표청구항

A thermal protection system comprising: an aerobrake for use to assist in the return of a space vehicle from a geosynchronous earth orbit or higher to a low earth orbit for recovery, servicing and reuse, said aerobrake is subject to be folded from a retracted position to a deployed position where it

이 특허를 인용한 특허 (37)

  1. Fleeter, Richard; DeBra, Daniel B.; Gloyer, Paul; Wahl, Zeno; Goldstein, David, Aerobraking orbit transfer vehicle.
  2. Stokes, Peter Hedley, Apparatus for spacecraft.
  3. Stokes, Peter Hedley, Apparatus for spacecraft.
  4. Featherstone, Mark, Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods.
  5. Featherstone, Mark, Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods.
  6. Featherstone, Mark, Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods.
  7. Cussac Thibery,FRX, Braking shield for a spacecraft, and a satellite fitted therewith.
  8. Grillos, Emmanuel; Trimble, Dennis Arthur; Grose, Douglas Lewis, Composite structures for aerospace vehicles, and associated systems and methods.
  9. Grillos, Emmanuel; Trimble, Dennis Arthur; Grose, Douglas Lewis, Composite structures for aerospace vehicles, and associated systems and methods.
  10. Featherstone, Mark, Control surfaces for use with high speed vehicles, and associated systems and methods.
  11. Featherstone, Mark; Boelitz, Frederick W.; Ramsey, Roger E.; Biggs, David M., Control surfaces for use with high speed vehicles, and associated systems and methods.
  12. Kutter, Bernard Friedrich; Zegler, Frank Charles; Willey, Cliff E.; Lin, John K.; Ragab, Mohamed M.; Dew, Michael W., Cryogenic propellant depot and deployable sunshield.
  13. Kutter, Bernard Friedrich; Zegler, Frank Charles; Ragab, Mohamed R., Cryogenic propellant depot and integral sunshield.
  14. Koehler, Frederick; Cheng, Wing; Cheng, legal representative, Helen H., Device and method for providing radiation occlusion and aero-thermal protection.
  15. DiChiara, Jr.,Robert A., Flexible insulation blanket having a ceramic matrix composite outer layer.
  16. DiChiara, Jr., Robert A., Flexible insulation blanket having secondarily bonded ceramic matrix composite layer.
  17. Clark,Paul R.; Messinger,Ross H., Folding retractable protective dome for space vehicle equipment.
  18. Takeda, Fumihito; Yamashita, Masayuki; Ogawa, Junichi; Anji, Toshiyuki; Kawasaki, Yoshihiro, Heat insulating material.
  19. Richard D. Fleeter, High-energy to low-energy orbit transfer vehicle.
  20. Coleman, Michael Edward, Inflatable deceleration apparatus.
  21. Bianca, Jr., Daniel M.; Scribner, Valeda B.; Hartlage, John Jay; Mak, Howen; Kang, Sung H.; El Masri, Teofilo R.; Ly, Sara; Rust, III, Thomas; Smith, Brian K.; Zapf, Arthur R.; Villegas, Jesse C.; Nedjar, Rachid, Integrated articulating thermal isolation system and method.
  22. Thornton Janine M., Material assembly for an inflatable aerodynamic braking device for spacecraft deceleration and the like.
  23. Daniel E. Boss ; Richard K. Williams ; Scott R. Dobrusky, Metal felt laminate structures.
  24. Eggink, Roy Anthony; Eberhardt, David Scott, Method for manufacturing and attachment of wing fairings.
  25. Eggink, Roy Anthony; Eberhardt, David Scott, Method for manufacturing and attachment of wing fairings.
  26. DiChiara, Jr., Robert A., Method for secondarily bonding a ceramic matrix composite layer to a flexible insulation blanket and an insulation blanket produced thereby.
  27. Sawko Paul M. (San Jose CA) Calamito Dominic P. (Redondo Beach CA) Jong Anthony (Downey CA), Method to produce flexible ceramic thermal protection system resistant to high aeroacoustic noise.
  28. Douglas Michael Smith ; R. Ulrich Boes DE; Alok Maskara, Multilayer insulation composite.
  29. Goldstein, David; McDermott, Scott A.; Gloyer, Paul; Fleeter, Richard, Orbit transfer vehicle with support services.
  30. Wright, Richard J., Orbital debris mitigation system and method.
  31. Shockey, Donald A.; Erlich, David C.; Simons, Jeffrey W., Penetration resistant fabric structures and materials.
  32. Bezos, Jeffrey P.; Lai, Gary; Findlay, Sean R., Sea landing of space launch vehicles and associated systems and methods.
  33. Fleeter Richard D., Small satellite GEO-to-LEO orbit transfer vehicle.
  34. Gancedo Valentin Menendez,ESX, Substantially rigid thermally insulating panel and method for manufacturing it.
  35. Stone, William C., System for emergency crew return and down-mass from orbit.
  36. Smith, Douglas M., Thermally reflective layer-porous metal oxide film insulation composite.
  37. Doucette ; Jr. Jean J. ; Franchitto Anthony R., Three dimensionally reinforced ablative/insulative composite.
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