"Application of Nuclear Propulsion to the Mars Manned Landing Mission."

"Application of Nuclear Propulsion to the Mars Manned Landing Mission."

This report has been prepared to provide Aerojet management and the interested NASA offices with nuclear propulsion decision aid data. The primary intent of these analyses is to evaluate potential space missions which may utilize nuclear propulsion in an effort to determine the most desirable chara...

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Bibliographic Details
Main Author: Advanced Concepts, Reon Division, Aerojet-General Corporation.
Format: Electronic
Published: University of Alabama in Huntsville Archives
Subjects:
Documents
Online Access:http://libarchstor2.uah.edu/digitalcollections/items/show/2332
format Electronic
collection Saturn V Collection
building University of Alabama in Huntsville Archives
publisher University of Alabama in Huntsville Archives
topic Documents
spellingShingle Documents
"Application of Nuclear Propulsion to the Mars Manned Landing Mission."
Advanced Concepts, Reon Division, Aerojet-General Corporation.
fulltopic Documents
Mars (Planet)--Exploration
Nuclear rocket engines
Saturn Project (U.S.)
Spacecraft propulsion
Space flight to Mars
description This report has been prepared to provide Aerojet management and the interested NASA offices with nuclear propulsion decision aid data. The primary intent of these analyses is to evaluate potential space missions which may utilize nuclear propulsion in an effort to determine the most desirable characteristics of a nuclear propulsion system.
spelling "Application of Nuclear Propulsion to the Mars Manned Landing Mission."Advanced Concepts, Reon Division, Aerojet-General Corporation.Mars (Planet)--ExplorationNuclear rocket enginesSaturn Project (U.S.) Spacecraft propulsion Space flight to MarsThis report has been prepared to provide Aerojet management and the interested NASA offices with nuclear propulsion decision aid data. The primary intent of these analyses is to evaluate potential space missions which may utilize nuclear propulsion in an effort to determine the most desirable characteristics of a nuclear propulsion system.1967-03ReportsStill ImageTextspc_stnv_000104http://libarchstor2.uah.edu/digitalcollections/items/show/2332http://libarchstor2.uah.edu/digitalcollections/files/original/20/2332/spc_stnv_000104.pdfSaturn V CollectionBox 11, Folder 3University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000075_000118This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections.
title "Application of Nuclear Propulsion to the Mars Manned Landing Mission."
titleStr "Application of Nuclear Propulsion to the Mars Manned Landing Mission."
author Advanced Concepts, Reon Division, Aerojet-General Corporation.
author_facet Advanced Concepts, Reon Division, Aerojet-General Corporation.
id UAHsaturnv2332
url http://libarchstor2.uah.edu/digitalcollections/items/show/2332
_version_ 1790443372555534336

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