"Study of a fail-safe abort system for an actively cooled hypersonic aircraft" - Information and Links:

Study of a fail-safe abort system for an actively cooled hypersonic aircraft - Info and Reading Options

volume I--technical summary

"Study of a fail-safe abort system for an actively cooled hypersonic aircraft" was published by U.S. National Aeronautics and Space Administration in 1976 - Washington, it has 75 pages and the language of the book is English.


“Study of a fail-safe abort system for an actively cooled hypersonic aircraft” Metadata:

  • Title: ➤  Study of a fail-safe abort system for an actively cooled hypersonic aircraft
  • Author:
  • Language: English
  • Number of Pages: 75
  • Publisher: ➤  U.S. National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: Washington

“Study of a fail-safe abort system for an actively cooled hypersonic aircraft” Subjects and Themes:

Edition Specifications:

  • Pagination: x, 75 p. :

Edition Identifiers:

AI-generated Review of “Study of a fail-safe abort system for an actively cooled hypersonic aircraft”:


Read “Study of a fail-safe abort system for an actively cooled hypersonic aircraft”:

Read “Study of a fail-safe abort system for an actively cooled hypersonic aircraft” by choosing from the options below.

Search for “Study of a fail-safe abort system for an actively cooled hypersonic aircraft” downloads:

Visit our Downloads Search page to see if downloads are available.

Find “Study of a fail-safe abort system for an actively cooled hypersonic aircraft” in Libraries Near You:

Read or borrow “Study of a fail-safe abort system for an actively cooled hypersonic aircraft” from your local library.

Buy “Study of a fail-safe abort system for an actively cooled hypersonic aircraft” online:

Shop for “Study of a fail-safe abort system for an actively cooled hypersonic aircraft” on popular online marketplaces.



Find "Study Of A Fail-safe Abort System For An Actively Cooled Hypersonic Aircraft" in Wikipdedia