Non-nuclear NEP system testing

被引:0
|
作者
Hrbud, I [1 ]
Goodfellow, K [1 ]
Van Dyke, M [1 ]
Houts, M [1 ]
机构
[1] NASA, ERC Inc, MSFC Grp, Huntsville, AL 35812 USA
来源
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - STAIF 2003 | 2003年 / 654卷
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Safe Affordable Fission Engine (SAFE) test se ties Addresses Phase 1 Space Fission Systems issues in particular non-nuclear testing and system integration issues leading to the testing and non-nuclear demonstration of a 400-kW fully integrated flight unit. The first part of the SAFE 30 test series demonstrated operation of the simulated nuclear core and heat pipe system. Experimental data acquired in a number of different test scenarios will validate existing computational models, demonstrated system flexibility (fast start-ups, multiple start-ups/shut downs), simulate predictable failure modes and operating environments. The objective of the second part is to demonstrate an integrated propulsion system consisting of a core, conversion system and a thruster where the system converts thermal heat into jet power. This end-to-end system demonstration sets a precedent for ground testing of nuclear electric propulsion systems. The paper describes the SAFE 30 end-to-end system demonstration and its subsystems.
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页码:533 / 539
页数:7
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