Keywords = Internal Ballistics
Investigation of Dual-Thrust Rocket Motor with Sonic Flow through an Intermediate Nozzle

Volume 16, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015, May 2015, Pages 1-14

Amr M. El-Nady; Ahmed M. Sarhan; Mohamed A. Al-Sanabawy; Mahmoud Y. Mohamed


Dual-Thrust Rocket Motor with an intermediate Nozzle at the condition of higher boosting pressure than the sustaining pressure

Volume 16, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 16 – May 26 - 28, 2015, May 2015, Pages 1-15

Amr M. El-Nady; Ahmed M. Sarhan; Mohamed A. Al-Sanabawy; Mahmoud Y. Mohamed


Modeling of End-Burning Solid Propellant Gas Generator

Volume 15, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013, May 2013, Pages 1-16

A. E. Makled; W. B. El-hasumi


PREDICTION OF HYBRID COMBUSTION BOUNDARY LAYER PARAMETERS

Volume 12, ASAT Conference, 29-31 May 2007, May 2007, Pages 1-15

A. EL-S MAKLED


CONTROL OVER BLAST WAVE AT EXIT POINT OF SUPER-SONIC PROJECTILE

Volume 9, ASAT Conference, 8-10 May 2001, May 2001, Pages 1-11

Abu-Elkhair M. S.; Sherif H. A.; Said S. M.


HYBRID PROPELLANT ROCKET MOTOR

Volume 8, ASAT Conference, 4-6 May 1999, May 1999, Pages 1-15

Frantitek LUDVIK