Published November 1979 | Version v1
Report Open

Dynamic Isotope Power System (DIPS) Applications Study. Volume II. Nuclear Integrated Multimission Spacecraft (NIMS) design definition. Final report

Creators

Description

The design requirements for the Nuclear Integrated Multimission Spacecraft. (NIMS) are discussed in detail. The requirements are a function of mission specifications, payload, control system requirements, electric system specifications, and cost limitations

Availability note (English)

MF available from INIS under the Report Number; Available from NTIS., PC A11/MF A01.

Files

11552652.pdf

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Additional details

Publishing Information

Imprint Pagination
227 p.
Report number
DOE/ET/3267--1(Vol.2)

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
11552652
Subject category
S07: ISOTOPES AND RADIATION SOURCES;
Descriptors DEI
COMPATIBILITY; COST; FEASIBILITY STUDIES; RADIOISOTOPE BATTERIES; RADIOISOTOPE HEAT SOURCES; SAFETY; SPACE VEHICLES; SPACECRAFT POWER SUPPLIES; SPECIFICATIONS
Descriptors DEC
DIRECT ENERGY CONVERTERS; ELECTRONIC EQUIPMENT; ENERGY SOURCES; POWER SUPPLIES

Optional Information

Secondary number(s)
GESD--79SDS4228(Vol.2).