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EFFECT OF OXIDIZER PARTICLE ORIENTATION ON BURNING RATES OF COMPOSITE PROPELLANTS
EFFECT OF OXIDIZER PARTICLE ORIENTATION ON BURNING RATES OF COMPOSITE PROPELLANTS
2016
Hiroshi Hasegawa
Mihoko Fukunaga
Koki Kitagawa
Toru Shimada
Keywords:
Particle
Aerospace engineering
Burn rate (chemistry)
Rocket propellant
Chemistry
Propellant
Composite number
Correction
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