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http://dx.doi.org/10.5139/JKSAS.2005.33.10.075

High-Speed Wind Tunnel Test on Rocket Booster Separation  

Ra, Seung-Ho (한국항공우주연구원 열/공력그룹)
Kim, In-Sun (한국항공우주연구원 열/공력그룹)
Ok, Ho-Nam (한국항공우주연구원 열/공력그룹)
Oh, Bum-Seok (한국항공우주연구원 기술경영그룹)
Lee, Joon-Ho (한국항공우주연구원 기술경영그룹)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.33, no.10, 2005 , pp. 75-81 More about this Journal
Abstract
Jettison, grid and CTS test are widely used for the store and stage separation studies. This is an introductory paper on the experimental methodology and typical results of grid and CTS test used for the Korean 3-stage sounding rocket development. Thirteen separation trajectories were evaluated in the ONERA S2MA wind tunnel at Mach numbers of 2.0 and 2.8. The test result was applied as the basic database for the design of optimized separation device.
Keywords
High Speed Wind Tunnel Test; Booster Separation; Grid Test; CTS Test; Captive Trajectory System;
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  • Reference
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