Adapter (rocketry)

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In rocketry, an adapter is a hollow cylindrical[1][failed verification] 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.