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Dtic Ad0827403%3a Altitude Developmental Testing Of The J 2 Rocket Engine In Propulsion Engine Test Cell (j 4) (test J4 1801 10) by Defense Technical Information Center

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1DTIC AD0827403: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-10)

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Five nonfiring propellant pump performance tests of the J-2 rocket engine were conducted in Test Cell J-4 of the Large Rocket Facility. The tests were accomplished during test period J4-1801-10 at pressure altitudes of approximately 100,000 ft to evaluate the effects of low fuel pump inlet pressure on pump operating characteristics (tests 10A through 10D) and to determine the effects of spinup with dry pumps on test 10E. In the first four tests, liquid nitrogen was utilized as the operating fluid in the oxidizer system for safety reasons and to prevent engine firing on any test. Thrust chamber and turbine components were thermally conditioned before each performance test.

“DTIC AD0827403: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-10)” Metadata:

  • Title: ➤  DTIC AD0827403: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-10)
  • Author: ➤  
  • Language: English

“DTIC AD0827403: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-10)” Subjects and Themes:

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The book is available for download in "texts" format, the size of the file-s is: 35.98 Mbs, the file-s for this book were downloaded 68 times, the file-s went public at Sun Dec 01 2019.

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