Back to Search
Start Over
Direct Formulation of Bipropellant Thruster Performance for Quantitative Cold-Flow Diagnostic
- Source :
- Journal of Propulsion and Power. 37:842-849
- Publication Year :
- 2021
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2021.
-
Abstract
- We present a straightforward formulation predicting the characteristic velocity and specific impulse for bipropellant thrusters as a direct function of injection conditions, propellant combination,...
- Subjects :
- Propellant
animal structures
Materials science
Mechanical Engineering
Aerospace Engineering
Hypergolic propellant
Mechanics
Heat transfer coefficient
Characteristic velocity
law.invention
Fuel Technology
Space and Planetary Science
law
Mass flow rate
Specific impulse
Chemical equilibrium
Combustion chamber
Subjects
Details
- ISSN :
- 15333876
- Volume :
- 37
- Database :
- OpenAIRE
- Journal :
- Journal of Propulsion and Power
- Accession number :
- edsair.doi...........5249c6568ec6053b975dc626686ecf30
- Full Text :
- https://doi.org/10.2514/1.b38310