Injection thrust termination and modulation in solid rockets
- 1 November 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (11), 2036-2038
- https://doi.org/10.2514/3.2730
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Engineering Relations for Heat Transfer and Friction in High-Velocity Laminar and Turbulent Boundary-Layer Flow Over Surfaces With Constant Pressure and TemperatureTransactions of the American Society of Mechanical Engineers, 1956
- Oscillating Airfoils at High Mach NumberJournal of the Aeronautical Sciences, 1953