Space Stats

Second stage - One RD-0210 engine fails at T+510 sec, resulting in flight path deviation, automatic shutoff of launch vehicle.

Payload propulsion system failed

Upper stage failure.

First-stage engine failure caused the rocket to crash 15 km from the pdad.

First stage failure.

T+51s payload shroud failed. Second stage continued but third stage failed to ignite.

First stage - 1 x RD-253 fire beginning at T+ 0.02 sec, rocket crashed near pad.

Block D upper stage did not fire and payload did not attain earth orbit,

Third stage failed.

First stage failure.

Second stage failed 267 seconds after launch.

Third stage failure

First stage hydraulics failure. A faulty valve led to a hydraulic leak. Vehicle destructed at T+383 seconds

Fourth stage control system malfunction after third stage collided with fourth stage.

Block D lost LOX due to valve defect.

Block D control system failure.

First orbital launch attempt made by China. The program distributor in the second stage broke down. The rocket crashed into the earth within view of the launch site after 69 seconds of flight.

First stage malfunction.

Launch vehicle failed to orbit - unknown cause.