The Stardust Mission has as its primary objective the acquisition and retur
n of cometary samples, which represents the first sample return from outsid
e of the Earth-moon system. The passage from deep space to the surface of t
he Earth is accomplished via a sample return capsule (SRC). The design of t
he capsule required a cooperative effort between Lockheed Martin, the prime
contractor, and multiple NASA field centers. The coordinated design proces
s that was undertaken to produce the Stardust SRC, in particular the re-ent
ry related systems, is described.