𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Simulative Study on the Erosive Burning of Solid Rocket Motors

✍ Scribed by Yamada, K. ;Goto, M. ;Ishikawa, N.

Book ID
127126957
Publisher
American Institute of Aeronautics and Astronautics
Year
1976
Tongue
English
Weight
923 KB
Volume
14
Category
Article
ISSN
0001-1452

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πŸ“œ SIMILAR VOLUMES

The effects of thermal gradients on Perf
The effects of thermal gradients on Performance of End-Burning Rocket Motors
✍ Robert D. Irvine πŸ“‚ Article πŸ“… 1990 πŸ› John Wiley and Sons 🌐 English βš– 500 KB

## Abstract The effect of a non‐uniform temperature distribution on the thrust‐time performance of an end‐burning solid propellant rocket motor charge is examined. It is shown that non‐planar surfaces develop. For some classes of temperature distribution, the effect of these non‐planar surfaces os

Research on the Crack Mechanism of High-
Research on the Crack Mechanism of High-Burning-Rate Propellant in the solid rocket motor
✍ D. A. Wang; N. F. Wang; G. M. Qin πŸ“‚ Article πŸ“… 1995 πŸ› John Wiley and Sons 🌐 English βš– 406 KB

## Abstract Through the analysis and calculation to the flow field in the solid rocket motor using high‐burning‐rate 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