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Dtic Ad0824273%3a Altitude Developmental Testing Of The J 2 Rocket Engine In Propulsion Engine Test Cell (j 4) (test J4 1801 02) by Defense Technical Information Center

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1DTIC AD0824273: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-02)

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Four firings, and one engine start to expiration of the ignition phase timer, of the Rocketdyne J-2 rocket engine were conducted in Test Cell J- 4. The firings were accomplished during test period J4-1801-02 at pressure altitudes from 97,000 to 106,000 ft at engine start. The objectives of the test were to evaluate S-IVB/S-V start condition effects on (1) gas generator and augmented spark igniter chamber ignition characteristics and (2) fuel pump stall characteristics during start tank blowdown for J-2 engine J-2052. Engine thermal conditions predicted for the J-2 engine flight configuration first burn, and restarts after one and two orbits, were simulated.

“DTIC AD0824273: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-02)” Metadata:

  • Title: ➤  DTIC AD0824273: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-02)
  • Author: ➤  
  • Language: English

“DTIC AD0824273: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-02)” Subjects and Themes:

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The book is available for download in "texts" format, the size of the file-s is: 40.21 Mbs, the file-s for this book were downloaded 91 times, the file-s went public at Sun Dec 01 2019.

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