Jump to content

LR105

From Wikipedia, the free encyclopedia
(Redirected from Rocketdyne LR-105)
An LR105 Atlas sustainer engine on display at the Air Zoo.

The LR105 is a liquid-fuel rocket engine that served as the sustainer engine for the Atlas rocket family.[1][2][3] Developed by Rocketdyne in 1957 as the S-4,[4][5][6] it is called a sustainer engine because it continues firing after the LR89 booster engines have been jettisoned, providing thrust during the ascent phase.[7]

Description

[edit]

The LR105 is a liquid-propellant engine using RP-1/LOX. The engine operates on a gas-generator cycle, where a small portion of the propellant is burned in a gas generator to drive the turbopumps, which supply the engine with fuel and oxidizer.

The engine was designed to be throttleable, meaning its thrust could be adjusted during flight to optimize performance. The LR105 also features regenerative cooling, where RP-1 fuel is circulated through cooling channels in the engine's nozzle and combustion chamber before being injected into the combustion process, preventing overheating and improving efficiency.

Versions

[edit]

The LR105 engine underwent several upgrades over its operational life, leading to multiple variants:[1][8][9][10][3]

Version Year Thrust (kN) Specific impulse (s) Burn Time (s) Details
LR105-3 1957 375.00 308 Atlas A, Atlas B
XLR105-5 1958 363.20 309 335 Atlas-Able, Atlas B, Atlas-Centaur, Atlas D, Atlas-Agena, Atlas LV-3B
LR105-5 1958 386.40 316 430 Atlas-Centaur, Atlas E, Atlas-Agena, Atlas F, Atlas SLV-3
LR105-7 1963 386.40 316 266 Atlas Agena, Atlas F, Atlas H, Atlas G, Atlas I

See also

[edit]

References

[edit]
  1. ^ a b Wade, Mark (2019). "LR105-3". Encyclopedia Astronautica. Retrieved 2024-10-12.
  2. ^ "Convair SM-65 Atlas". National Museum of the US Air Force.
  3. ^ a b McCutcheon, Kimble D. (2022). "U.S. Manned Rocket Propulsion Evolution - Part 5: The Atlas Missile". Aircraft Engine Historical Society. Retrieved 2024-10-12.
  4. ^ Bilstein, Roger E. (August 1999). Stages to Saturn: A Technological History of the Apollo/Saturn Launch Vehicle. DIANE Publishing. p. 119. ISBN 978-0-7881-8186-3.
  5. ^ Wade, Mark (2019). "S-4 engine". Encyclopedia Astronautica. Retrieved 2024-10-12.
  6. ^ Wade, Mark (2019). "Rocketdyne". Encyclopedia Astronautica. Retrieved 2024-10-12.
  7. ^ Swopes, Bryan (2024-08-27). "Rocketdyne LR105-NA-5 | This Day in Aviation". Retrieved 2024-10-12.
  8. ^ Wade, Mark (2019). "LR105-5". Encyclopedia Astronautica. Retrieved 2024-10-12.
  9. ^ Wade, Mark (2019). "XLR105-5". Encyclopedia Astronautica. Retrieved 2024-10-12.
  10. ^ Wade, Mark (2019). "LR105-7". Encyclopedia Astronautica. Retrieved 2024-10-12.