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From Earth to Orbit: An assessment of transportation options [PDF]
The report assesses the requirements, benefits, technological feasibility, and roles of Earth-to-Orbit transportation systems and options that could be developed in support of future national space programs.
Blond, Edmund +9 more
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Performance Analysis of a Kerosene/Gaseous Oxygen Liquid Rocket Engine
Engineering ProceedingsOne of the most widely used rocket propulsion systems that uses liquid propellants is the liquid rocket engine. Due to their high density and specific impulse, liquid fuels and oxidizers are preferred.
Saravanan Ganesan +4 more
doaj +1 more source
In-situ propellant rocket engines for Mars mission ascent vehicle [PDF]
When comtemplating the human exploration of Mars, many scenarios using various propulsion systems have been considered. One propulsion option among them is a vehicle stage with multiple, pump fed rocket engines capable of operating on propellants ...
Roncace, Elizabeth A.
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Device for suppressing sound and heat produced by high-velocity exhaust jets Patent [PDF]
, 1966 Device for adding water to high velocity exhaust jets to reduce velocity, noise, and ...
Kramer, F.
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Reusable rocket engine intelligent control system framework design, phase 2 [PDF]
Elements of an advanced functional framework for reusable rocket engine propulsion system control are presented for the Space Shuttle Main Engine (SSME) demonstration case.
Anderson, Ron +3 more
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Visualization of acoustic radiation from the rocket propulsion system in the first seconds of the launch [PDF]
, 2019 Galyna Ivanovna Sokol +4 more
openalex +1 more source
Nuclear gas core propulsion research program [PDF]
Viewgraphs on the nuclear gas core propulsion research program are presented. The objectives of this research are to develop models and experiments, systems, and fuel elements for advanced nuclear thermal propulsion rockets.
Anghaie, Samim +2 more
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CFD Evaluation of a New Centrifugal Pump Concept for Rocket Propulsion
, 2022 Ion Mălăel, Bucur Ioana
openalex +2 more sources
Concepts for the design of an antimatter annihilation rocket [PDF]
Matter-antimatter annihilation is considered for spacecraft propulsion. Annihilation produces considerably more energy per unit mass of propellant than any other known means of energy production. An antimatter annihilation rocket requires several systems
Morgan, D. L., Jr.
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Electric propulsion technology [PDF]
The advanced electric propulsion program is directed towards lowering the specific impulse and increasing the thrust per unit of ion thruster systems. In addition, electrothermal and electromagnetic propulsion technologies are being developed to attempt ...
Finke, R. C.
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