Results 111 to 120 of about 28,947 (287)

Thermal and acceleration load analysis of new 122 mm rocket propellant grain [PDF]

, 2016
Nikola Gligorijević, Saša Antonović, Saša Živković, Bojan Pavković, Vesna Rodić   +4 more
openalex   +1 more source

Performance Evaluation of Hybrid Propellant Rocket Engine

, 2023
V. Siva, S. Vikramasuriyan, S. Mugundhan
openalex   +1 more source

Numerical modeling of translational and rotational vibrations of a solid-propellant rocket motor on a test stand during firing tests [PDF]

, 2023
М. Т. Lysenko, V.V. Rohulin, A.V. Demchenko, I.B. Bezkrovnyi, R. V. Kalnysh   +4 more
openalex   +1 more source

Nonlinear combustion instability in liquid-propellant rocket motors Final report [PDF]

Mathematical models of nonlinear combustion instabilities in liquid propellant rocket ...
Burstein, S. Z., Chinitz, W., Schechter, H. S.   +2 more
core   +1 more source

CSM programs SM RCS propellant quantity gaging systems program [PDF]

, 1971
Computer program calculates actual and useable remaining propellant quantities as required in positive expulsion rocket engine propellant feed system. Program establishes relationship between helium system pressures and temperatures and propellant weight
Cox, G. R., Reynolds, R. G.
core   +1 more source

Beyond the horizon: Why space biology is the next great innovation opportunity

Experimental Physiology, EarlyView.
Carina Kern, Keith Siew
wiley   +1 more source

A simulation study of fracture toughness for a solid rocket motor contains a cracked propellant grain: Consideration of gas impingement effect [PDF]

, 2022
Tingyu Wang, Jinsheng Xu, Xiong Chen
openalex   +1 more source

Liquid rocket performance computer model with distributed energy release Interim final report, 15 Aug. 1969 - 15 Aug. 1970 [PDF]

Liquid propellant rocket engine performance computer program with distributed energy ...
Campell, D. T., Chadwick, W. D., Combs, L. P.   +2 more
core   +1 more source

Enhanced thermal performance and hydrochloric acid gas (HCl) emission mitigation in ammonium perchlorate (AP)-Based solid propellants with potassium permanganate (KMnO4)/AP dual oxidisers

Atmospheric Environment: X
The conventional propellant used in rocket boosters and tactical missiles commonly utilises ammonium perchlorate (AP). However, the release of harmful chloride fumes resulting from the combustion of AP during rocket launches contributes to a 1 % increase
Izzat Najmi Yaacob, Ezanee Gires, Adi Azrif Basri, Kamarul Arifin Ahmad, Kamsani Kamal, Nor Afizah Salleh, Suraya Shahedi, Fikri Rasih, Zakwan Azizi, Sharul Sham Dol, Norkhairunnisa Mazlan   +10 more
doaj   +1 more source

Development of low cost ablative nozzles for solid propellant rocket motors, volume 1 Final report [PDF]

Evaluating low cost ablative materials for use in large solid propellant rocket ...
Laramee, R. C., Mathis, J. R.
core   +1 more source