Cores – Page 0

Engine failure at T+33 seconds resulted in loss of vehicle

Successful first-stage burn and transition to second stage, maximal altitude 289 km. Harmonic oscillation at T+5 minutes Premature engine shutdown at T+7 min 30 s. Failed to reach orbit.

Residual stage-1 thrust led to collision between stage 1 and stage 2.

Initially scheduled for 23–25 Sep, carried dummy payload – mass simulator, 165 kg (originally intended to be RazakSAT.

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Stage Expended

First flight of Dragon

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Suffered engine out at T+1:19 but primary mission successful

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