Published January 1, 1991 | Version v1
Journal article

Shielding analysis for a manned Mars rover powered by an Sp-100 type reactor

  • 1. Institute for Space Nuclear Power Studies, Department of Chemical and Nuclear Engineering, University of New Mexico Albuquerque, NM, 87131 (USA)

Description

Shield design is one of the most crucial tasks in the integration of a nuclear reactor power system to a manned Mars rover. A multilayered W and LiH shield is found to minimize the shield mass and satisfy the dose rate limit of 30 rem/y to the rover crew. The effect on dose rate of tungsten layers thicknesses and position within the lithium hydride shields is investigated. Due to the large cross section for the W (n,γ) reaction, secondary gammas become a significant radiation source. The man-rated shield mass for the Mars rover vehicle is correlated to the reactor thermal power. The correlation fits to within 9% of the calculated shield mass and results in an uncertainty of <4% in the overall rover mass. The shield mass varied from 8600 kg to 20580 kg for a reactor thermal power of 100 to 1000 kWt, respectively

Additional details

Publishing Information

Journal Title
AIP Conference Proceedings
Journal Volume
217
Journal Issue
1
Series
AIP Conf. Proc.
Journal Page Range
347-354
ISSN
0094-243X
CODEN
APCPC

Conference

Title
8. symposium on space nuclear power systems.
Dates
6-10 Jan 1991.
Place
Albuquerque, NM (USA).

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
22077744
Subject category
S21: SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS;
Resource subtype / Literary indicator
Conference
Descriptors DEI
LITHIUM HYDRIDES; MARS SPACE PROBES; RADIATION DOSES; RADIATION HAZARDS; SHIELDING; SPACE POWER REACTORS; SPACE VEHICLES; TUNGSTEN
Descriptors DEC
ALKALI METAL COMPOUNDS; ELEMENTS; HAZARDS; HEALTH HAZARDS; HYDRIDES; HYDROGEN COMPOUNDS; LITHIUM COMPOUNDS; METALS; MOBILE REACTORS; POWER REACTORS; REACTORS; TRANSITION ELEMENTS

Optional Information

Secondary number(s)
CONF-910116--.