Results 121 to 130 of about 38,554 (239)

In-situ propellant rocket engines for Mars mission ascent vehicle [PDF]

open access: yes
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.
core   +1 more source

Concepts for the design of an antimatter annihilation rocket [PDF]

open access: yes
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.
core   +1 more source

Electric propulsion technology [PDF]

open access: yes
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.
core   +1 more source

Reusable rocket engine intelligent control system framework design, phase 2 [PDF]

open access: yes
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
core   +1 more source

Rocket propulsion

open access: yesNature, 1960
Barrère, Marcel   +3 more
openaire   +3 more sources

A cermet fuel reactor for nuclear thermal propulsion [PDF]

open access: yes
Work on the cermet fuel reactor done in the 1960's by General Electric (GE) and the Argonne National Laboratory (ANL) that had as its goal the development of systems that could be used for nuclear rocket propulsion as well as closed cycle propulsion ...
Kruger, Gordon
core   +1 more source

Advanced oxygen-hydrocarbon rocket engine study [PDF]

open access: yes
Preliminary identification and evaluation of promising liquid oxygen/ hydrocarbon (LO2/HC) rocket engine cycles is reported. A consistent and reliable data base for vehicle optimization and design studies, to demonstrate the significance of propulsion ...
Obrien, C. J.
core   +1 more source

Home - About - Disclaimer - Privacy