Future NTP Development Synergy Leveraged from Current J-2X Engine Development
Creators
- 1. Liquid Engine and Main Propulsion Systems Branch, NASA Marshall Space Flight Center, AL 35812 (United States)
Description
This paper is a discussion of how the many long-lead development elements required for the realization of a future nuclear thermal propulsion (NTP) system can be effectively leveraged from the ongoing work being conducted on the J-2X engine program for the Constellation Program. Development studies conducted to date for NTP forward planning have identified a number of technical areas that will require advancement to acceptable technology readiness levels (TRLs) before they can be utilized in NTP system development. These include high-temperature, high-area ratio nozzle extension; long-life, low-NPSP turbomachinery; and low-boiloff propellant management, and a qualified nuclear fuel element. The current J-2X program is working many of these areas that can be leveraged to support NTP development in a highly compatible and synergistic fashion. In addition to supporting technical development, there are other programmatic issues being worked in the J-2X program that can be leveraged by a future NTP development program. These include compliance with recently-evolved space system requirements such as human-rating, fault tolerance and fracture control. These and other similar mandatory system requirements have been adopted by NASA and can result in a significant technical impact beyond elevation of the root technologies required by NTP. Finally, the exploitation of experience, methodologies, and procedures developed by the J-2X program in the areas of verification, qualification, certification, altitude simulation testing, and facility definition will be especially applicable to a future NTP system. The similarities in system mission (in-space propulsion) and operational environment (vacuum, zero-gee) between J-2X and NTP make this highly synergistic. Thus, it can be shown that the collective benefit of leveraging experience and technologies developed during the J-2X program can result in significant savings in development cost and schedule for NTP
Additional details
Identifiers
- DOI
- 10.1063/1.2845011;
Publishing Information
- Journal Title
- AIP Conference Proceedings
- Journal Volume
- 969
- Journal Issue
- 1
- Journal Page Range
- p. 526-532
- ISSN
- 0094-243X
- CODEN
- APCPCS
Conference
- Title
- 12. conference on thermophysics applications in microgravity; 1. symposium on space resource utilization; 25. symposium on space nuclear power and propulsion; 6. conference on human/robotic technology and the vision for space exploration; 6. symposium on space colonization; 5. symposium on new frontiers and future concept
- Acronym
- Space Technology and Applications International Forum-STAIF 2008
- Dates
- 10-14 Feb 2008
- Place
- Albuquerque, NM (United States)
INIS
- Country of Publication
- United States
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 39061612
- Subject category
- S42: ENGINEERING;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- COMPUTERIZED SIMULATION; CONTROL; FRACTURES; HEAT ENGINES; MOON; NASA; NUCLEAR FUELS; PROPULSION; PROPULSION SYSTEMS; SPACE PROPULSION REACTORS; TURBOMACHINERY
- Descriptors DEC
- ENERGY SOURCES; ENGINES; EQUIPMENT; FAILURES; FUELS; MACHINERY; MATERIALS; MOBILE REACTORS; NATIONAL ORGANIZATIONS; POWER REACTORS; PROPULSION REACTORS; REACTOR MATERIALS; REACTORS; SATELLITES; SIMULATION; SPACE POWER REACTORS; US ORGANIZATIONS
Optional Information
- Notes
- (c) 2008 American Institute of Physics