Downloads & Free Reading Options - Results
Dtic Ad0876657%3a Altitude Developmental Testing Of The J 2s Rocket Engine In Rocket Development Test Cell J 4 (tests J4 1001 16 Through 20) by Defense Technical Information Center
Read "Dtic Ad0876657%3a Altitude Developmental Testing Of The J 2s Rocket Engine In Rocket Development Test Cell J 4 (tests J4 1001 16 Through 20)" by Defense Technical Information Center through these free online access and download options.
Books Results
Source: The Internet Archive
The internet Archive Search Results
Available books for downloads and borrow from The internet Archive
1DTIC AD0876657: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell J-4 (Tests J4-1001-16 Through -20)
By Defense Technical Information Center
Fourteen firings of the Rocketdyne J-2S rocket engine (S/N J-115) were conducted during test periods J4-1001-16 through -20 between March 10 and May 19, 1970. The major objectives of these tests were: (1) development of a throttling capability using a variable-position tapoff valve for thrust control; (2) demonstration of satisfactory idle-mode operation (both pre- and post-main stage) over a wide range of fuel and oxidizer pump inlet pressures; (3) determine the suitability of the S-IVB propellant recirculation system to prefire condition propellants and prechill engine propellant pumps; and (4) determine steady-state engine performance during main-stage operation. All major objectives were satisfactorily accomplished.
“DTIC AD0876657: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell J-4 (Tests J4-1001-16 Through -20)” Metadata:
- Title: ➤ DTIC AD0876657: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell J-4 (Tests J4-1001-16 Through -20)
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC AD0876657: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell J-4 (Tests J4-1001-16 Through -20)” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Franklin, D E - ARO INC ARNOLD AFS TN - *LIQUID PROPELLANT ROCKET ENGINES - ALTITUDE CHAMBERS - CAPTIVE TESTS - COMBUSTION CHAMBER GASES - CONTROLLABLE THRUST ROCKET ENGINES - DUCT INLETS - HIGH ALTITUDE - LAUNCH VEHICLES - LIQUID ROCKET FUELS - LIQUID ROCKET OXIDIZERS - PRESSURE - PROPELLANT CONTROL - STAGING - THROTTLING - THRUST - TURBOPUMPS
Edition Identifiers:
- Internet Archive ID: DTIC_AD0876657
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 44.00 Mbs, the file-s for this book were downloaded 67 times, the file-s went public at Fri Dec 06 2019.
Available formats:
Abbyy GZ - Archive BitTorrent - DjVuTXT - Djvu XML - Item Tile - Metadata - OCR Page Index - OCR Search Text - Page Numbers JSON - Scandata - Single Page Processed JP2 ZIP - Text PDF - chOCR - hOCR -
Related Links:
- Whefi.com: Download
- Whefi.com: Review - Coverage
- Internet Archive: Details
- Internet Archive Link: Downloads
Online Marketplaces
Find DTIC AD0876657: Altitude Developmental Testing Of The J-2S Rocket Engine In Rocket Development Test Cell J-4 (Tests J4-1001-16 Through -20) at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Buy “Dtic Ad0876657%3a Altitude Developmental Testing Of The J 2s Rocket Engine In Rocket Development Test Cell J 4 (tests J4 1001 16 Through 20)” online:
Shop for “Dtic Ad0876657%3a Altitude Developmental Testing Of The J 2s Rocket Engine In Rocket Development Test Cell J 4 (tests J4 1001 16 Through 20)” on popular online marketplaces.
- Ebay: New and used books.