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Space Nuclear Propulsion (SNP) Material Property HandbookThe National Aeronautics and Space Administration’s (NASA’s) Space Nuclear Propulsion (SNP) project aims to demonstrate the feasibility of nuclear thermal propulsion (NTP) as a thrust mechanism for spacecraft. An initial Demonstration Rocket for Agile Cislunar Operations (DRACO) launch will serve as a test of the technology in Earth’s orbit. Future work may involve the development of an NTP engine and spacecraft design with the capability to transport astronauts from Earth to Mars and back safely, though NTP has other potential uses too.
Document ID
20240004217
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Handbook (NHB)
Authors
Justin L Milner
(Glenn Research Center Cleveland, United States)
Peter Karkos
(HX5 (United States) Fort Walton Beach, Florida, United States)
Jessica Jane Bowers
(HX5 (United States) Fort Walton Beach, Florida, United States)
Date Acquired
April 9, 2024
Publication Date
August 5, 2024
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
SNP-HDBK-0008
ST-23
Funding Number(s)
WBS: 039889
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
External Peer Committee
Keywords
Nuclear Thermal Propulsion
Space Nuclear Propulsion
Thermophysical Properties
Thermal Properties
Material Properties
Metals and Metallic Materials
Nonmetallic Materials
Composite Materials
Chemistry and Materials
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