Launch Failure

Liftoff Time (GMT)

15:17:00

Wednesday August 25, 1965

Watch Replay

24/7 Coverage

Mission Details

Launch Notes

Third stage ignited while still attached to the second stage.

OSO-C

Wiki

The main body of the spacecraft consists of a wheel of aluminum alloy separated into nine wedge-shaped compartments. Five of these compartments contain apparatus for five experiments not requiring solar orientation. The remaining four compartments house the electronic controls, batteries, telemetry equipment, and radio-command equipment. Each wheel compartment provides approximately 1000 cubic inches of volume, and each wheel experiment can weigh up to approximately 45 pounds. The wheel also contains three extendable arms which are folded down around the third stage of the launch vehicle during the launch phase. When the spacecraft is injected into orbit, the arms are extended which increases the effective diameter of the wheel from 1.1 meters to 2.4 meters.

Low Earth Orbit

1 Payload

Rocket

Retired
Delta C

Active 1963 to 1967


Rocket

Height: 31m

Payload to Orbit

LEO: 410 kg

GTO: 82 kg

Liftoff Thrust

667 Kilonewtons

Stages

3

Launch Site

SLC-17B

Cape Canaveral SFS, Florida, USA

Fastest Turnaround

20 days 2 hours

Stats

Delta C


8th

Mission

5th

Mission of 1965

1965


78th

Orbital launch attempt