Throttling of rocket propulsion systems represents means for obtaining precise control of ballistic missile and space vehicle flight characteristics, and for enabling single rocket engine to accommodate propulsive requirements of different maneuvers; review of principal mission areas in which throttling is required and summary of major throttling techniques.
Toward variable-thrust liquid-rocket engine
Astronautics Aerospace Eng
Astronautics and Aerospace Engineering ; 1 , n 11
1963
5 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
VARIABLE-THRUST LIQUID PROPELLANT ROCKET ENGINES
AIAA | 1963
|Liquid rocket engine : thrust chamber parametrical modeling
TIBKAT | 2019
|Variable Thrust Rocket Engines
AIAA | 1960
|Britain's first variable-thrust rocket
Engineering Index Backfile | 1956