Adapter (rocketry)

In rocketry, an adapter is a hollow cylindrical[1] or conical segment[2] which provides a sound aerodynamic and structural connection, either between rocket stages (referred to as an interstage adapter) or between a spacecraft and the top rocket stage (referred to as a payload adapter). It may shroud and protect vulnerable systems such as electrics or machinery of rocket engines/spacecraft from weather or noise caused by running engines. It is discarded during staging.

Examples of Rocket Stages featuring an interstage adapter:

Examples of Rocket Stages featuring a payload adapter:

References

  1. United States. Patent Office (December 1952). Official Gazette of the United States Patent Office. U.S. Patent Office.
  2. Wiley J. Larson; Linda K. Pranke (1999). Human Spaceflight: Mission Analysis and Design. McGraw-Hill. ISBN 978-0-07-236811-6.
  3. "The Launch of Atlas-Centaur 5". 2 March 2015.
  4. "Centaur - Mission Planners Guide (NASA CR-154970)" (PDF). General Dynamics Convair Aerospace Division. 1 August 1971. Archived (PDF) from the original on 8 January 2022.
  5. "Atlas Launch System Mission Planner's Guide, Atlas V Addendum (AVMPG)" (PDF). Lockheed Martin. 1 December 1999.
  6. McCutcheon, Kimble D. (3 August 2022). "U.S. Manned Rocket Propulsion Evolution Part 8.20: The Saturn V S-II".
  7. McCutcheon, Kimble D. (3 August 2022). "U.S. Manned Rocket Propulsion Evolution Part 8.30: The Saturn S-IVB Stage".
  8. "NASA's Space Launch System Launch Vehicle Stage Adapter Ready for Thermal Insulation Application". 30 August 2017. Retrieved 14 September 2022.
  9. "Universal Stage Adapter (USA)". Retrieved 14 September 2022.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.