EFFECT OF POST-CHAMBER ON COMBUSTION EFFICIENCY IN HYBRID ROCKET MOTORS
Last updated: 24 Dec 2024
10.21608/asat.2013.24425
Rocket motor, Hybrid propulsion, Regression rate
A.
Makle
Egyptian Armed Forces.
A-N.
Zaye
Egyptian Armed Forces.
H.
Abdalla
Egyptian Armed Forces.
M.
EI-Senbawi
Egyptian Armed Forces.
10
10th International Conference On Aerospace Sciences & Aviation Technology
4497
2003-05-01
2019-01-14
2003-05-01
253
266
2090-0678
2636-364X
https://asat.journals.ekb.eg/article_24425.html
https://asat.journals.ekb.eg/service?article_code=24425
17
Original Article
737
Journal
International Conference on Aerospace Sciences and Aviation Technology
https://asat.journals.ekb.eg/
EFFECT OF POST-CHAMBER ON COMBUSTION EFFICIENCY IN HYBRID ROCKET MOTORS
Details
Type
Article
Created At
22 Jan 2023