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Thrust structure

From EverybodyWiki Bios & Wiki

The thrust structure, also sometimes referred to as thrust barrel or thrust frame, is a load bearing structure inside a rocket which transfers the thrust generated by one or several rocket engines to the body of the rocket, usually formed by the fuselage.[1]

Usually, the thrust structure is either composed of:

  • An inverted, hollow truncated cone stiffened with Stringers[3][4] if one single or several nearby engines need to be connected to the body of the rocket.

Examples

References

  1. Keller, R. B., Jr. (1 October 1979). NASA Space Vehicle Design Criteria (SP-8126): Glossary of terms and table of conversion factors used in design of chemical propulsion systems (PDF). p. 72. Archived from the original on 7 August 2022. Unknown parameter |url-status= ignored (help)CS1 maint: Multiple names: authors list (link) Search this book on
  2. Kimble D. McCutcheon (3 August 2022). "U.S. Manned Rocket Propulsion Evolution Part 8.10: The Saturn V S-IC Stage - S-IC Overview". Archived from the original on 5 June 2022. Unknown parameter |url-status= ignored (help)
  3. 3.0 3.1 Kimble D. McCutcheon (3 August 2022). "U.S. Manned Rocket Propulsion Evolution Part 8.30: The Saturn S-IVB Stage - S-IVB Structure". Archived from the original on 5 August 2022. Unknown parameter |url-status= ignored (help)
  4. Kimble D. McCutcheon (3 August 2022). "U.S. Manned Rocket Propulsion Evolution Part 8.20: The Saturn V S-II Stage - S-II Description". Archived from the original on 5 June 2022. Unknown parameter |url-status= ignored (help)


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