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Dtic Ad0871088%3a Altitude Developmental Testing Of The J 2s Rocket Engine In Rocket Development Test Cell (j 4) (tests J4 1001 08 Through 10 And J4 1001 12 Through 14) by Defense Technical Information Center
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1DTIC AD0871088: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell (J-4) (Tests J4-1001-08 Through -10 And J4-1001-12 Through -14)
By Defense Technical Information Center
Ten idle-mode firings of the J-2S rocket engine S/N J-112 were conducted during test periods J4-1001-08 through J4-1001-10, and J4-1001-12 through J4-1001-14 between September 2 and October 15, 1969, in Rocket Development Test Cell (J-4) of the Engine Test Facility. The primary objectives of these firings were to determine engine idle-mode operating characteristics at various engine mixture ratios utilizing a new noncompartmented injector. Engine performance, as indicated by characteristic velocity, was 120 percent higher than experienced with previous compartmented injector designs at nominal pump inlet conditions. Total accumulated engine idle-mode operation was 1408.2 sec.
“DTIC AD0871088: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell (J-4) (Tests J4-1001-08 Through -10 And J4-1001-12 Through -14)” Metadata:
- Title: ➤ DTIC AD0871088: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell (J-4) (Tests J4-1001-08 Through -10 And J4-1001-12 Through -14)
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC AD0871088: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell (J-4) (Tests J4-1001-08 Through -10 And J4-1001-12 Through -14)” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Kunz, C H - ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN - *LIQUID PROPELLANT ROCKET ENGINES - ALTITUDE CHAMBERS - CAPTIVE TESTS - CONTROLLABLE THRUST ROCKET ENGINES - CRYOGENIC PROPELLANTS - FUEL INJECTION - FUEL INJECTORS - HIGH ALTITUDE - HYDROGEN - INTERIOR BALLISTICS - LAUNCH VEHICLES - MIXTURES - OXYGEN - PERFORMANCE(ENGINEERING) - PRESSURE - PROPELLANT CONTROL - SIMULATION - TEMPERATURE - TURBOPUMPS - VELOCITY
Edition Identifiers:
- Internet Archive ID: DTIC_AD0871088
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 50.36 Mbs, the file-s for this book were downloaded 70 times, the file-s went public at Thu Dec 05 2019.
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