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
β¦ LIBER β¦
Liquid rocket engines for large thrust: Present and future
β Scribed by A. Sergienko
- Book ID
- 103498618
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 407 KB
- Volume
- 29
- Category
- Article
- ISSN
- 0094-5765
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