Design and testing of an airbag landing attenuator system for a generic crew return vehicle

Collection of Technical Papers - 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar

Volumn , Issue , 2005, Pages 146-168

  Cooper, Michelle ^a   Sinclair, Robert ^a,c   Sanders, John ^a   Frigerio, Jacapo ^b  

^a Irvin Aerospace Inc   (United States)

^b LOCKHEED MARTIN SPACE SYSTEMS COMPANY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; ELECTRIC ATTENUATORS; FLIGHT DYNAMICS; ORIFICES; VENTS;

CONTROL FLOW RATE; CREW RETURN VEHICLES; IMPACT ATTENUATION AIRBAGS; VENTING AIRBAGS;

PLANETARY LANDERS;

EID: 29144458191     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1616     Document Type: Conference Paper

References (6)

1. Cooper, M.S., Taylor, A.P., Farhall, R.J., Irvin document GIP 99-1100 Test Plan for Initial System Testing
2. Cooper, M.S., Farhall, R.J., Irvin document GIP 99-1091 Test Procedure for Airbag Orifice Testing
3. Sanders, J., Cooper, M.S., Taylor, A.P., Irvin Document GIR 93-198 Airbag Orifice Test and Simulation Calibration Report
4. Sanders, J., Cooper, M.S., Taylor, A.P., Irvin Document GIR 85-1331 Analysis and Design Evolution Report for the Lockheed Martin Reentry Vehicle Simulator Airbag Attenuation System
5. Cooper, M.S., Taylor, A.P., Farhall, R.J., Irvin Document GIP 99-1089 Test Plan for Impact Attenuation Testing at Yuma Proving Ground
6. Sanders, J., Cooper, M.S., Taylor, A.P., Farhall, R.J., Irvin Document GIR 93-201 Test Report for Airbag Impact Attenuation Testing at Yuma Proving Ground