Inside and Out: The Space Suits and Escape Systems

  • Luc van den Abeelen
Chapter
Part of the Springer Praxis Books book series (PRAXIS)

Abstract

ESA started the development of a European EVA suit in 1986, after work on Hermes had begun, but before official Europeanization of the project. At that time, Europe was essentially without any experience in building pressure suits for space applications. French industry did study pressure suits: the DTI 100 and -101 in the early 1960s [1] and for Mirage fighter pilots in the 1960s an early 1980s [2] but building a dedicated space suit was something new for Europe. As the Hermes programme developed, the concept for an IVA suit became dependent on the choice for its escape system.

Keywords

Landing Gear Operational Envelope Seat Booster Pressure Suit Escape System 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

References

  1. 1.
    Atmosphere d’une cabine spatiale et sortie extra-véhiculaire, L’Aéronautique et l’Astronautique, No 131, 4/1988, p 9Google Scholar
  2. 2.
    Etude de faisabilite des scaphandres AIV et AEV pour Hermes, RE-201, Intertechnique, August 1986Google Scholar
  3. 3.
    Spaceshots, Flight International, 19 December 1987, p 38Google Scholar
  4. 4.
    ESA/IPC(88)53, 20 April 1988, 12402Google Scholar
  5. 5.
    Italy’s Role in European Space Suit Program Discussed, JPRS-EST-90-011, 21 May 1990Google Scholar
  6. 6.
    US Spacesuits, Kenneth S. Thomas and Harold J. McMann, Praxis Publishing Ltd, 2006, pp 319–321Google Scholar
  7. 7.
    The Soviet/Russian spacesuit history: Part III – The European connection, A. Ingemar Skoog, Isaak P. Abramov, Acta Astronautica, volume 60, Issue 12, June 2007, pp 1002–1014Google Scholar
  8. 8.
    ESA proposed ‘Octopus’ robot for use with space station, JPRS-ELS-87-013, 17 March 1987, p 15Google Scholar
  9. 9.
    Hermes quick reference, ESA/D/STS/H April 1992, p 32Google Scholar
  10. 10.
    Hermes, Final Frontier, February 1989, p 37Google Scholar
  11. 11.
    Hermes Escape System, J. Colrat et al, Proceedings of the International Symposium on Europe in Space – The Manned System, Strasbourg, 25–29 April 1988, ESA SP-299, October 1988, p 269–274Google Scholar
  12. 12.
    French boost space plane’s safety, Steve Conner, New Scientist, 10 July 1986, p 28Google Scholar
  13. 13.
    Hermes Programme Evolution File, GMV SA, 2032/93, p IV.4–10Google Scholar
  14. 14.
    Compte rendu de reunion d’avancement Hermes du 3 juillet 1987, CNES H-CR-0-0002-CNE, 3 July 1987Google Scholar
  15. 15.
    Hermes Definition Program Begins: First Manned Mission Set for 1998, Aviation Week & Space Technology, 11 April 1988, p 51Google Scholar
  16. 16.
    AFP Sciences, No 606, 31 March 1988, pp 14–17Google Scholar
  17. 17.
    ESA/PB-ARIANE/MIN/89, 29 April 1988, HAEU ESA-12702Google Scholar
  18. 18.
    Private notes on the International Symposium on Europe in Space: The Manned Space System, Strasbourg, 25–29 April 1988 by Stephane ChenardGoogle Scholar
  19. 19.
    Cabine ejectable jusqu’a Mach 7 et 50 km d’altitude pour Hermes, Air & Cosmos, 7 May 1988Google Scholar
  20. 20.
    ESA/IPC(88)53, 20 April 1988, HAEUR ESA-12402Google Scholar
  21. 21.
    Flying Qualities of the Hermes Spaceplane and the Shape Definition Process. E. Raillon et al, ESA Journal, Vol 16, 1992, p 422Google Scholar
  22. 22.
    Hermes Crew Escape Module, H.P. Nguyen, F. Frank, IAF-80-060, IAF Congress, Bangalore, India, 8–15 October 1988Google Scholar
  23. 23.
    New Hermes Escape System Proposed, Theo Pirard, Spaceflight, Vol. 30, December 1988, p 467Google Scholar
  24. 24.
    CEM type A/LB Synthesis Report, MBB H-NT-1-1080-MBB, 1 December 1989Google Scholar
  25. 25.
    Cabine pointe avant sans visibilite – Sauvegarde par tour d’extraction, rapport technique d’etude du concept, CNES H-NT-1-0042-CNES, 4 November 1988Google Scholar
  26. 26.
    Hermes Crew Escape Module Configuration Studies, H.P. Nguyen et al, IAF-89-616, AIF Congress, Malaga, Spain, 7–12 October 1989Google Scholar
  27. 27.
    Hermes Crew Escape Means comparison of development options, Aerospatiale, H-NT-1-621-AS, 29 October 1990Google Scholar
  28. 28.
    Rafale and EFA share Martin-Baker seat, Flight International, 12–18 September 1990, p 26Google Scholar
  29. 29.
    Système de sauvetage: “la Qualité pour la dernière chance”, Louis Lemaignen, Olivier Thomas, Qualité Espace, Dassault, undatedGoogle Scholar
  30. 30.
    Hermes Encapsulated Ejection Seat, pre-development study final report, Martin-Baker, December 1989Google Scholar
  31. 31.
    Contribution au choix du moyen de sauvegarde de léquipage de l’avion spatial Hermes, CNES H-NT-0-0018-CNES, 7 November 1989Google Scholar
  32. 32.
    Sieges ejectables pour Hermes, Air & Cosmos, 6 January 1990Google Scholar
  33. 33.
    L’URSS va aider Dassault pour Hermes, Air & Cosmos, 10 February 1990, p 49Google Scholar
  34. 34.
    L’Italie fournira les sieges ejectables d’Hermes, Air & Cosmos, 26 November 1990, p 54Google Scholar
  35. 35.
    Zvezda IVA Suit technical description, Buran technology transfer option, Dassault H-NT-1P-1002-AMD, 25 July 1990Google Scholar
  36. 36.
    Soviet Ejection Seat for Buran Shuttle Qualified for Deployment at Up to Mach 4, Aviation Week & Space Technology, 10 June 1990, p 44Google Scholar
  37. 37.
    ESA/IPC(2)122, 7 September 1992, HAEU ESA-16018Google Scholar
  38. 38.
    Hermes System Definition File (HSDF), H-DF-0-01-HPD, March 1992, pp 240–244Google Scholar
  39. 39.
    Hermes Functional File H-DF-1-001-EHS, 17 March 1993, p 95Google Scholar

Copyright information

© Springer International Publishing Switzerland 2017

Authors and Affiliations

  • Luc van den Abeelen
    • 1
  1. 1.HilversumThe Netherlands

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