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Title: NASA low power DIPS [Dynamic Isotope Power System] conceptual design requirements document

Abstract

This document describes the requirements for a low power (0.5--1.0 kwe) Dynamic Isotope Power System (DIPS) for interplanetary and space exploration missions using the Mariner Mark II spacecraft. The reference mission used to establish these requirements was the Cassini orbiter mission to Saturn. Requirements specific to two other missions (Outer Planet Orbiter/Probe and Comet Nucleus Sample Return) are also included. A list of references used to develop these requirements is provided. 17 refs., 2 figs., 2 tabs.

Authors:
; ;
Publication Date:
Research Org.:
Rockwell International Corp., Canoga Park, CA (United States). Rocketdyne Div.
Sponsoring Org.:
USDOE
OSTI Identifier:
721000
Report Number(s):
DOE/NE/32129-T4
ON: TI91020262; IN: EID-00093
DOE Contract Number:
AC03-88NE32129
Resource Type:
Technical Report
Resource Relation:
Other Information: PBD: [1990]
Country of Publication:
United States
Language:
English
Subject:
07 ISOTOPES AND RADIATION SOURCES; 30 DIRECT ENERGY CONVERSION; SPACECRAFT POWER SUPPLIES; DESIGN; SPACE VEHICLES; THERMOELECTRIC GENERATORS; MISSION ANALYSIS; BUDGETS; SPECIFICATIONS; NESDPS Office of Nuclear Energy Space and Defense Power Systems

Citation Formats

Johnson, G., Determan, W., and Otting, W.. NASA low power DIPS [Dynamic Isotope Power System] conceptual design requirements document. United States: N. p., 1990. Web. doi:10.2172/721000.
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Johnson, G., Determan, W., & Otting, W.. NASA low power DIPS [Dynamic Isotope Power System] conceptual design requirements document. United States. doi:10.2172/721000.
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Johnson, G., Determan, W., and Otting, W.. Mon . "NASA low power DIPS [Dynamic Isotope Power System] conceptual design requirements document". United States. doi:10.2172/721000. https://www.osti.gov/servlets/purl/721000.
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@article{osti_721000,
title = {NASA low power DIPS [Dynamic Isotope Power System] conceptual design requirements document},
author = {Johnson, G. and Determan, W. and Otting, W.},
abstractNote = {This document describes the requirements for a low power (0.5--1.0 kwe) Dynamic Isotope Power System (DIPS) for interplanetary and space exploration missions using the Mariner Mark II spacecraft. The reference mission used to establish these requirements was the Cassini orbiter mission to Saturn. Requirements specific to two other missions (Outer Planet Orbiter/Probe and Comet Nucleus Sample Return) are also included. A list of references used to develop these requirements is provided. 17 refs., 2 figs., 2 tabs.},
doi = {10.2172/721000},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Mon Jan 01 00:00:00 EST 1990},
month = {Mon Jan 01 00:00:00 EST 1990}
}
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Technical Report:
View Technical Report (0.94 MB)
DOI:  10.2172/721000
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