Thrust improvement with ablative insert nozzle extension
- 1 January 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 2 (1), 91-93
- https://doi.org/10.2514/3.22849
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Application of the Saderholm erosive burning model to nozzleless solid propellant rocket motorsJournal of Spacecraft and Rockets, 1984
- Transonic flowfield in a supersonic nozzle with small throat radius of curvature.AIAA Journal, 1969
- Flow phenomena and convective heat transfer in a conical supersonic nozzle.Journal of Spacecraft and Rockets, 1967
- Detection of oblique shocks in a conical nozzle with a circular-arc throat.AIAA Journal, 1966