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Source: The Open Library
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1The rationale/benefits of nuclear thermal rocket propulsion for NASA'S lunar space transportation system
By Stanley K. Borowski
“The rationale/benefits of nuclear thermal rocket propulsion for NASA'S lunar space transportation system” Metadata:
- Title: ➤ The rationale/benefits of nuclear thermal rocket propulsion for NASA'S lunar space transportation system
- Author: Stanley K. Borowski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“The rationale/benefits of nuclear thermal rocket propulsion for NASA'S lunar space transportation system” Subjects and Themes:
- Subjects: ➤ Nuclear propulsion - Nuclear engine for rocket vehicles - Lunar bases - Propulsion system configurations - Mission planning - Space transportation system - Thrust-weight ratio - Reusable launch vehicles - Lunar orbital rendezvous
Edition Identifiers:
- The Open Library ID: OL15408794M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Lunar orbit rendezvous
Lunar orbit rendezvous (LOR) is a process for landing humans on the Moon and returning them to Earth. It was utilized for the Apollo program missions in
Space rendezvous
rendezvous (/ˈrɒndeɪvuː/) is a set of orbital maneuvers during which two spacecraft, one of which is often a space station, arrive at the same orbit and
Earth orbit rendezvous
vehicle in low Earth orbit. It was considered as an alternative to direct ascent but ultimately rejected in favor of lunar orbit rendezvous (LOR) for NASA's
Saturn C-3
different rendezvous possibilities. The alternatives included Earth-orbital rendezvous (EOR), lunar-orbital rendezvous (LOR), Earth and lunar rendezvous, and
Joseph Francis Shea
Apollo program, helping to lead NASA to the decision in favor of lunar orbit rendezvous and supporting "all up" testing of the Saturn V rocket. While sometimes
Apollo Lunar Module
Lunar Module (LM /ˈlɛm/), originally designated the Lunar Excursion Module (LEM), was the lunar lander spacecraft that was flown between lunar orbit and
John Houbolt
an aerospace engineer credited with leading the team behind the lunar orbit rendezvous (LOR) mission mode, a concept that was used to successfully land
Lunar orbit
only a few orbital trajectories possible for indefinite frozen orbits. These would be useful for long-term stays in LLO. Most lunar low orbits below 100 km
Lanyue
carrier rocket, and subsequently acquire lunar orbit under its own power. It then will await a lunar orbit rendezvous with and docking by the separately launched
Apollo program
OCLC 30520885. Hansen, James R. (1999). Enchanted Rendezvous: John C. Houbolt and the Genesis of the Lunar-Orbit Rendezvous Concept (PDF). Monographs in Aerospace