Some anomalies in the dependence of the specific pulse of rocket propellants on the aluminum content
β Scribed by D. B. Lempert; G. N. Nechiporenko; S. I. Soglasnova
- Book ID
- 111472438
- Publisher
- Pleiades Publishing
- Year
- 2008
- Tongue
- English
- Weight
- 137 KB
- Volume
- 2
- Category
- Article
- ISSN
- 1990-7931
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
## Abstract Through the analysis and calculation to the flow field in the solid rocket motor using highβburningβrate propellant, the authors believe that the existence of pressure difference between the inside and outside of the propellant tube causes the propellant crack. In this paper, the design
Melt casting processed samples of Bi,Sr,CaCu,O,+d were prepared with oxygen contents ranging from kO.126 to 6=0.22 and characterized by electrical resistance and AC-susceptibility. The r, of this compound is shifted reversibly between 75 and 95 K by annealing in Ar and/or O2 atmospheres for various