Pratt & Whitney XLR-129

Cut-drawing of XLR-129 demonstrator engine

The XLR-129 was an American rocket engine design that would have used liquid hydrogen and liquid oxygen propellants.[1] It was developed by Pratt & Whitney and initially was to develop 250,000 lbs of thrust. It featured an expanding nozzle in order to tune performance over a wide range of altitudes.

The XLR-129 was designed to be reusable and was initially paid for by the US Air Force, for a 1960s program called ISINGLASS which was to be a manned rocket plane that was intended for surveillance overflights. For the Space Shuttle an attempt was made to increase the thrust to 350,000 lbs, but in the end Rocketdyne's Space Shuttle Main Engine was used instead.[2]

The XLR-129 program was never completed, no complete engine was ever produced, but many systems were developed and tested.[3]

References

  1. ↑
  2. ↑
  3. ↑ "Air Force Reusable Rocket Engine Program XLR129-P-1. Volume 1". US Air Force. January 1971. Retrieved 2010-05-22.
This article is issued from Wikipedia - version of the 10/8/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.