Space shuttle orbiter drag parachute system

摘要

The desire to increase landing safety margins for the United States Space Shuttle Orbiter led to the decision to implement a Drag Parachute System into the Orbiter Vehicle. This paper presents the design, development, and implementation of this high profile/high visibility system. The main focus will be related to the parachute system. A Brief description of the mechanical, structural, thermal, avionics, and pressure integrity system modifications required to accommodate a parachute is included.