Cryogenic rocket calorimeter chamber experiments and heat transfer simulations
- 13 July 1998
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An Eulerian-Lagrangian approach to spray combustion modeling for liquid bi-propellant rocket enginesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Heat transfer characteristics of H2/O2-combustion chambersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Comparison of rocket nozzle heat transfer calculation methodsJournal of Spacecraft and Rockets, 1978