Results 161 to 170 of about 9,371 (228)

Key attributes of nitrocellulose-based energetic materials and recent developments. [PDF]

open access: yesHeliyon
Abdul Rahim KS   +6 more
europepmc   +1 more source

Propellants and Combustion [PDF]

open access: yes, 1962
Penner, Stanford S.
core  

On porous liquid propellant rocket engine injectors

Aerospace Science and Technology, 2008
A novel injection concept for cryogenic liquid propellant rocket engines has been tested and verified successfully using an optically accessible combustion chamber. The injector consists of a porous faceplate made from sinter metal and five LOX posts arranged in a classical parallel showerhead configuration.
Lux, Johannes   +2 more
exaly   +2 more sources

Liquid-Propellant Rocket Engines

2012
The liquid-propellant rocket engine has the characteristics that allow it to deliver thrust at a high-performance level, with an efficiency and operational flexibility that enables a number of mission applications to go forward. Monopropellant and bipropellant versions of this category of engine are discussed in some detail in this chapter.
exaly   +2 more sources

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