Oxygen Generation Using Catalytic Nano/Micromotors. [PDF]
Naeem S +13 more
europepmc +1 more source
High energy propellants - A continuing bibliography with indexes [PDF]
Bibliography on solid, liquid, and hybrid high energy propellants and oxidizers, propellant handling and storage, toxicity and hazards, and safety ...
core +1 more source
Valve, normally closed, titanium Pyronetics model 1426 [PDF]
Performance tests of the explosive actuated, normally closed titanium valve 1426, are outlined. The valves are used to control hydrazine flow in a monopropellant thruster. Data cover pressure tests, internal and external leakage tests, flow control tests,
Avalos, E.
core +1 more source
Catalytic decomposition of hydroxylamine nitrate and hydrazine nitrate using Ru/ZSM-5 catalyst under mild reaction conditions. [PDF]
Zhang Z +6 more
europepmc +1 more source
The hard start phenomena in hypergolic engines. Volume 2: Combustion characteristics of propellants and propellant combinations [PDF]
The combustion characteristics of hypergolic propellants are described. A research project was conducted to determine if the reaction control system engine propellants on Apollo spacecraft undergo explosive reaction when subjected to conditions present ...
Miron, Y., Perlee, H. E.
core +1 more source
Numerical Study of Flow Boiling of ADN-Based Liquid Propellant in a Capillary. [PDF]
Liu X, Su G, Yao Z, Yan Z, Yu Y.
europepmc +1 more source
Recent Advances in MEMS-Based Microthrusters. [PDF]
Liu B, Li X, Yang J, Gao G.
europepmc +1 more source
Experimental Study on Microwave-Assisted Ignition and Combustion Characteristics of ADN-Based Liquid Propellant. [PDF]
Hou Y, Yu Y, Liu X, Chen J, Zhang T.
europepmc +1 more source
The concept of the Mars airplane was developed as a potential vehicle for unmanned Mars exploration. It is suggested that its most appropriate use would be as an unmanned adjunct to a manned mission.
French, J. R.
core +1 more source
Effect of Microwave Power and Gas Flow Rate on the Combustion Characteristics of the ADN-based Liquid Propellant. [PDF]
Pan S +7 more
europepmc +1 more source

