Deployable Landing Leg Concept for Crew Exploration Vehicle

By: Administration (Nasa), National Aeronaut

The NASA Exploration program is investigating the merits of land landing concepts for the Crew Exploration Vehicle (CEV). Four options are under investigation: retro-rockets which fire and slow the vehicle before contact with the landing surface, deployable crushable material which deploys just before landing and crushes during land contact, airbags which deploy just before landing and deflate during land contact, and deployable legs which deploy before landing and contain material that absorbs energy during land contact. The purpose of the present work is to determine the effectiveness of the deployable leg concept. To accomplish this goal, structural models of the deployable leg concept are integrated with the Crew Model (CM) and computational simulations are performed to determine vehicle and component loadings and acceleration levels. Details of the modeling approach, deployable leg design, and resulting accelerations are provided. Lawrence, Charles and Solano, Paul and Bartos, Karen Glenn Research Center NASA/TM-2007-214705, E-15930 WBS 843515.02.01.03.05.08.04 CREW EXPLORATION VEHICLE; SPACECRAFT LANDING; SPACECRAFT DESIGN; WATER LANDING; SPACECRAFT MODELS; AIR BAG RESTRAINT DEVICES; DISPLACEMENT; ACCELERATION; FINITE ELEMENT METHOD; SIMULATION; CENTER OF GRAVITY

• Format: Paperback
• Language: English
• ISBN: B08DSNCSWM
• ISBN13: 9798670291323
• Release Date: January 1
• Publisher: Independently Published
• Length: 26 Pages
• Weight: 0.19 lbs.
• Dimensions: 0.1" x 8.5"