Human Mars Entry, Descent and Landing Architecture Study: Rigid Decelerators

Polsgrove, Tara P ; Percy, Thomas K ; Garcia, Jay C ; Cianciolo, Alicia D ; Samareh, Jamshid A ; Lugo, Rafael A ; Robertson, Edward A ; Cerimele, Chris J ; Sostaric, Ron R ; Garcia, Joseph A

关键词: DESCENT;    MANNED MARS MISSIONS;    MISSION PLANNING;   

RP-ID  :  MSFC-E-DAA-TN60268

学科分类：天文学(综合)

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

Several technology investments are required to develop Mars human scale Entry, Descent, and Landing (EDL) systems. Studies play the critical role of identifying the most feasible technical paths and high payoff investments. The goal of NASA's Entry, Descent and Landing Architecture Study is to inform those technology investments. In Phase 1 of the study, a point design for one lifting-body-like rigid decelerator vehicle, was developed. In Phase 2, a capsule concept was also considered to determine how it accommodated the human mission requirements. This paper summarizes the concept of operations for both rigid vehicles to deliver a 20-metric ton (t) payload to the surface of Mars. Details of the vehicle designs and flight performance are presented along with a packaging, mass sizing, and a launch vehicle fairing assessment. Finally, recommended technology investments based on the analysis of the rigid vehicles are provided.