Dragon crew capsule

USA


Launch data:

Launch date 06 May 2015 (abort test)
Launch site CC
Launch vehicle   -
Mission 1e pad abort test
Dragon crew capsule

The Dragon capsule for SpaceX′s pad abort test seen inside a test chamber. Credit: SpaceX



Spacecraft data:

Prime contractor  SpaceX
Platform  
Operator SpaceX
Mass at launch   kg
Dry Mass  kg
Basic shape  Cyl-cone
Dimension (m) 
Solar array  
Stabilization  
DC power  

Mission details:



The eight SuperDracos ignited simultaneously and reached maximum thrust, propelling the spacecraft off the pad.

After half a second of vertical flight, Crew Dragon pitched toward the ocean and continued its controlled burn. The SuperDraco engines throttled to control the trajectory based on real-time measurements from the vehicle′s sensors. Dragon traveled from 0-100 mph in 1.2 seconds, reaching a max velocity of 345 mph.



The abort burn was terminated once all propellant was consumed, and Dragon coasted to its highest point. The trunk was jettisoned and the spacecraft began a slow rotation with its heat shield pointed toward the ground again.

Small parachutes, called drogues, were deployed first following trunk separation.



Once the drogue parachutes stabilized the vehicle, three main parachutes deployed and further slowed the spacecraft before splashdown.

Less than two minutes after ignition, Dragon splashed down in the Atlantic Ocean downrange of the launch pad.


External links:


Astrophilately covers:

Dragon Pad Abort Test

Dragon Pad Abort Test, cancel Cape Canaveral.



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