๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Design criteria for film cooling for small liquid-propellant rocket engines.

โœ Scribed by HOWELL, J. C.; OBERSTONE, J.; STECHMAN, R. C.


Book ID
120341798
Publisher
American Institute of Aeronautics and Astronautics
Year
1969
Tongue
English
Weight
961 KB
Volume
6
Category
Article
ISSN
0022-4650

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Design, calibration and error analysis o
โœ Qin Xing; Jun Zhang; Min Qian; Zhenyuan Jia; Baoyuan Sun ๐Ÿ“‚ Article ๐Ÿ“… 2011 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 786 KB

Small thrust liquid pulsed rocket engines operating in pulsed mode have gained a good reputation in attitude control applications for their potential reliability and efficiency. However, the pulsed characteristic creates a difficult measurement problem. In this paper, a novel thrust dynamometer with