The Vision for Space Exploration, established by President Bush in January 2004, has prompted NASA to begin development of a new spacecraft, the Crew Exploration Vehicle. This vehicle, named Orion, will possess the capabilities to travel to the space station, the moon, and eventually Mars. The purpose of this research was to analyze the wake characteristics behind the Orion capsule and provide
... [Show full abstract] NASA with main and drogue parachute deployment strategies and recommendations. The facility used for this research was the Subsonic Wind Tunnel at the United States Air Force Academy. Four planes, 3.35 Orion diameters by 3.72 Orion diameters, located at 5.5, 6.5, 10.5 and 12 diameters aft of the Orion model were surveyed with the Orion model at 0 and 17 degree angles of attack and Mach 0.475 and Mach 0.35 tunnel velocity. The results from the wake survey indicated three significant trends for all planes and configurations tested. The lowest measured dynamic pressure recovery fraction was similar at each angle of attack and Mach number. The displacement of the wake center at 17 degrees angle of attack increased linearly to the side of the Orion model from 0.62 diameters at Mach 0.35 to 1.3 diameters at Mach 0.472. The radius of the wake displayed dynamic characteristics by increasing for regions of high pressure recovery fractions and decreasing for regions of low pressure recovery fractions as distance aft of the Orion model increased. The results provided sufficient data to recommend continued development with the six diameter bridle on the drogue chute, a drogue skirt that can withstand dynamic pressures that are 71% of the freestream dynamic pressure, and a triple drogue chute configuration. It is also recommended that the main parachute selection consider both the total bridle/line length and the wake radius in a triple chute configuration. This effort was sponsored by NASA Johnson Space Center.