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기술보고서

기술보고서 게시판 내용
타이틀	Aero-Structural Assessment of an Inflatable Aerodynamic Decelerator
저자	Sheta, Essam F.;; Venugopalan, Vinod;; Tan, X. G.;; Liever, Peter A.;; Habchi, Sami D.
Keyword	AERODYNAMIC BRAKES;; ATMOSPHERIC ENTRY;; DESCENT;; INFLATABLE STRUCTURES;; LANDING AIDS;; MARS (PLANET); PAYLOADS;; SIMULATION;; SYSTEMS ANALYSIS;; TOROIDS
URL	http://hdl.handle.net/2060/20100031172
보고서번호	NASA/CR-2010-216731
발행년도	2010
출처	NTRS (NASA Technical Report Server)
ABSTRACT	NASA is conducting an Entry, Descent and Landing Systems Analysis (EDL-SA) Study to determine the key technology development projects that should be undertaken for enabling the landing of large payloads on Mars for both human and robotic missions. Inflatable Aerodynamic Decelerators (IADs) are one of the candidate technologies. A variety of EDL architectures are under consideration. The current effort is conducted for development and simulations of computational framework for inflatable structures.