국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Analyses of Noise from Reusable Solid Rocket Motor (RSRM) Firings
저자	Gee, Kent L.;; Kenny, R. Jeremy;; Jerome, Trevor W.;; Neilsen, Tracianne B.;; Hobbs, Christopher M.;; James, Michael M.
Keyword	ACOUSTICS;; LAUNCHING;; REUSABLE ROCKET ENGINES;; ROCKET ENGINE NOISE;; SOLID PROPELLANT ROCKET ENGINES;; SPACECRAFT LAUNCHING;; VIBRATIONAL STRESS
URL	http://hdl.handle.net/2060/20130000695
보고서번호	M12-2219
발행년도	2012
출처	NTRS (NASA Technical Report Server)
ABSTRACT	NASA''s Space Launch Vehicle (SLS) program has chosen the Reusable Solid Rocket Motor V (RSRMV) as the booster system for initial flights. Lift off acoustics continue to be a consideration in overall vehicle vibroacoustic evaluations and launch pad modifications. Work started with the Ares program to understand solid rocket noise mechanisms is continuing through SLS program in conjunction with BYU/Blue Ridge Research Consulting.