Abstract
This article discusses the issues involved in launching humans with an electromagnetic railgun launcher. The acceleration tolerance limits are discussed based on prior work by the National Aeronautics and Space Administration (NASA) and USAF. A potential application is described, wherein an emergency recovery system for astronauts on the lunar surface could be used for launch into lunar orbit for subsequent rendezvous and recovery aboard a parent vehicle. Tradeoffs between tolerable astronaut Gee-loads and launcher parameters are discussed, and the possibility of direct drive with batteries is considered. The tentative conclusion, subject to further analysis, is that such a system may be possible but that comparison with alternatives is required before a decision could be made to undertake such a development.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
