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Performance Analysis of Axial-Injection, End-Burning Hybrid Rocket Propulsion System
- Source :
- Journal of Spacecraft and Rockets. 57:1408-1413
- Publication Year :
- 2020
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2020.
-
Abstract
- Although several investigations have been performed regarding the fundamental physics of axial-injection, end-burning hybrid rocket motors, investigations into the mission performance of a propulsi...
- Subjects :
- Physics
020301 aerospace & aeronautics
business.product_category
integumentary system
Spacecraft propulsion
business.industry
Aerospace Engineering
macromolecular substances
02 engineering and technology
Characteristic velocity
Propulsion
01 natural sciences
010305 fluids & plasmas
Chamber pressure
Propellant mass fraction
0203 mechanical engineering
Rocket
Space and Planetary Science
0103 physical sciences
Fundamental physics
Aerospace engineering
business
Delta-v
Subjects
Details
- ISSN :
- 15336794 and 00224650
- Volume :
- 57
- Database :
- OpenAIRE
- Journal :
- Journal of Spacecraft and Rockets
- Accession number :
- edsair.doi...........cb7852db2cde4990f57a30be589828f1