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Dtic Ad0825574%3a Altitude Developmental Testing Of The J 2 Rocket Engine In Propulsion Engine Test Cell (j 4) (test J4 1801 08) by Defense Technical Information Center
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1DTIC AD0825574: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-08)
By Defense Technical Information Center
Four firings of the J-2 rocket engine were conducted in Test Cell J-4 of the Large Rocket Facility. The firings were accomplished during test period J4-1801-08 at pressure altitudes ranging from 92,500 to 107,000 ft at engine start. The objectives of the test were to evaluate S-IVB/S-V start condition effects on (1) engine start transients, (2) gas generator outlet temperature; (3) augmented spark igniter operation, and (4) fuel pump high level stall margin for J-2 engine S/N J-2052. The accumulated firing duration was 70.32 sec. Satisfactory engine operation was obtained.
“DTIC AD0825574: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-08)” Metadata:
- Title: ➤ DTIC AD0825574: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-08)
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC AD0825574: ALTITUDE DEVELOPMENTAL TESTING OF THE J-2 ROCKET ENGINE IN PROPULSION ENGINE TEST CELL (J-4) (TEST J4-1801-08)” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Simpson, J N - ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN - *LIQUID PROPELLANT ROCKET ENGINES - ALTITUDE CHAMBERS - CAPTIVE TESTS - FUEL PUMPS - GAS GENERATING SYSTEMS - HIGH ALTITUDE - LAUNCH VEHICLES - PERFORMANCE(ENGINEERING) - ROCKET IGNITERS - STALLING - STARTING - TIME
Edition Identifiers:
- Internet Archive ID: DTIC_AD0825574
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The book is available for download in "texts" format, the size of the file-s is: 44.22 Mbs, the file-s for this book were downloaded 84 times, the file-s went public at Sun Dec 01 2019.
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