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Air Force Reusable Rocket Engine Program XLR129-P-1. Demonstrator Engine design. Volume 1.


AD508757

Publication Date 1970
Personal Author Atherton, R. R.
Page Count 111
Abstract No abstract available.
Keywords
  • Liquid propellant rocket engines
  • Design
  • Liquefied gases
  • Oxygen
  • Hydrogen
  • Controllable-thrust rocket motors
  • Rocket nozzles
  • Life expectancy
  • Weight
  • Thrust
  • Throttling
  • Interfaces
  • Lr-129 engines
  • Xlr-129-p-1 engines
  • Reusable rocket engines
  • Nickel alloy inconel 625
  • Slot tube swirler injectors
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 81G - Rocket Engines & Motors
Corporate Authors Pratt and Whitney Aircraft, West Palm Beach, FL. Florida Research and Development Center.
Supplemental Notes See also Volume 2, AD-508 764.
Document Type Technical Report
Title Note Technical rept. 6 Nov 67-1 Dec 69.
NTIS Issue Number 198615
Contract Number
  • F04611-68-C-0002
Air Force Reusable Rocket Engine Program XLR129-P-1. Demonstrator Engine design. Volume 1.
Air Force Reusable Rocket Engine Program XLR129-P-1. Demonstrator Engine design. Volume 1.
AD508757

  • Liquid propellant rocket engines
  • Design
  • Liquefied gases
  • Oxygen
  • Hydrogen
  • Controllable-thrust rocket motors
  • Rocket nozzles
  • Life expectancy
  • Weight
  • Thrust
  • Throttling
  • Interfaces
  • Lr-129 engines
  • Xlr-129-p-1 engines
  • Reusable rocket engines
  • Nickel alloy inconel 625
  • Slot tube swirler injectors
  • Non Paid Delimited ADS
  • 81G - Rocket Engines & Motors
  • F04611-68-C-0002
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