Thrust-chamber technology for oxygen difluoride/diborane propellants
- 1 January 1971
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (1) , 4-14
- https://doi.org/10.2514/3.30210
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Application of space storable injector and chamber design criteria to spacecraft engine developmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969