NDLI: Nuclear electric propulsion stage requirements and description

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Nuclear electric propulsion stage requirements and description

Content Provider	NASA Technical Reports Server (NTRS)
Author	Phillips, W. M. Peelgren, M. L. Nsieh, T. M. Mondt, J. F. Kikin, G. M. Nakashima, A. M.
Copyright Year	1974
Description	The application of a nuclear electric propulsion (NEP) stage in the exploration of near-earth, cometary, and planetary space was discussed. The NEP stage is powered by a liquid-metal-cooled, fast spectrum thermionic reactor capable of providing 120 kWe for 20,000 hours. This power is used to drive a number of mercury ion bombardment thrusters with specific impulse in the range of 4000-5000 seconds. The NEP description, characteristics, and functional requirements are discussed. These requirements are based on a set of five coordinate missions, which are described in detail. These five missions are a representative part of a larger set of missions used as a basic for an advanced propulsion comparison study. Additionally, the NEP stage development plan and test program is outlined and a schedule presented.
File Size	1571928
Page Count	72
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19740023992
Archival Resource Key	ark:/13960/t85j29d0x
Language	English
Publisher Date	1974-08-01
Access Restriction	Open
Subject Keyword	Nuclear Engineering Comets Ion Engines Space Exploration Spacecraft Design Nuclear Electric Propulsion Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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