Results 141 to 150 of about 63,703 (327)
High performance dash on warning air mobile, missile system [PDF]
An aircraft-missile system which performs a high acceleration takeoff followed by a supersonic dash to a 'safe' distance from the launch site is presented.
Castellano, C. R. +2 more
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Upper Stage Liquid Propellant Rocket Engine: A Case Analysis [PDF]
, 2021 Daniel Soares de Almeida +2 more
openalex +1 more source
Operationally Efficient Propulsion System Study (OEPSS) data book. Volume 4: OEPSS design concepts [PDF]
This study was initiated to identify operations problems and cost drivers for current propulsion systems and to identify technology and design approaches to increase the operational efficiency and reduce operations costs for future propulsion systems. To
Farhangi, Shahram +2 more
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Design issues for lunar in situ aluminum/oxygen propellant rocket engines [PDF]
Design issues for lunar ascent and lunar descent rocket engines fueled by aluminum/oxygen propellant produced in situ at the lunar surface were evaluated.
Meyer, Michael L.
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Improved simulation of cryogenic fluid mixing at supercritical pressures. [PDF]
PLoS One, 2023 Omair M, Akay HU.
europepmc +1 more source
A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]
Sci RepLi T, He H, Yu N, Sun X, Cai G.
europepmc +1 more source
The design of a Mars Mission Vehicle that would have to be launched by two very heavy lift launch vehicles is described along with plans for a mission to Mars.
Hornung, R.
core +1 more source
Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Polymers (Basel)Chmielarek M +2 more
europepmc +1 more source
A Study of the Internal Two-Phase Flow in Gas-Centered Swirl Coaxial Injectors
, 2013 International audienceAn effective atomization of liquid is of importance in the performance of combustion engines. For liquid hydrocarbon rocket engines with a staged combustion cycle for high-power application, the Gas-Centered Swirl Coaxial (GCSC ...
Cartellier, Alain H. +5 more
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