Results 101 to 110 of about 148,565 (303)

Prediction of explosive yield and other characteristics of liquid propellant rocket explosions Final report [PDF]

open access: yes
Explosive hazards and yield predictions for liquid rocket ...
Bonzon, C. F.   +2 more
core   +1 more source

Current activities at IITRI on high- temperature protective coatings [PDF]

open access: yes
Heat resistant protective coatings for use in liquid propellant rocket ...
Hess, A. L.   +2 more
core   +1 more source

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

open access: yes
Liquid propellant rocket engine performance computer program with distributed energy ...
Campell, D. T.   +2 more
core   +1 more source

Analysis of liquid-propellant rocket engines designed by F. A. Tsander [PDF]

open access: yes
The development of the oxygen-gasoline OR-2 engines and the oxygen-alcohol GIRD-10 rocket engine is described. A result of Tsander's rocket research was an engineering method for propellant calculation of oxygen-propellant rocket engines that determined ...
Dushkin, L. S., Moshkin, Y. K.
core   +1 more source

Rocket propellant injector Patent [PDF]

open access: yes, 1960
Propellant injectors for rocket combustion ...
Mantler, R. L.
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

open access: yesAtmospheric 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   +10 more
doaj   +1 more source

Bipropellant and quadredundant valves, volume 1 Final report [PDF]

open access: yes
Performance tests on bipropellant and quadredundant propellant valves for rocket ...

core   +1 more source

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