Vela 5A/5B, OV5-5, OV5-6, OV5-9

Launch Success

Liftoff Time (GMT)

07:57:00

Friday May 23, 1969

Watch Replay

24/7 Coverage

Mission Details

Vela 5A/5B

Wiki

Vela was the name of a group of satellites developed as the Vela Hotel element of Project Vela by the United States to detect nuclear detonations to monitor compliance with the 1963 Partial Test Ban Treaty by the Soviet Union.

Highly Elliptical Orbit

2 Payloads

518 kilograms

OV5-6

Wiki

The satellite had an octagonal configuration, was spin-stabilized, and was placed in a moderately elliptical earth orbit (eccentricity - 0.670) by a Titan 3C on May 25, 1969. The purpose of the satellite was to monitor x-ray, electron, and proton radiation associated with solar activity in order to develop data handling techniques in near real-time for use by the Air Weather Service Forecast Center in forecasting solar flares.

1 Payload

23 kilograms

OV5-9

Wiki

The purpose of this octahedral satellite was to monitor solar activity by measuring solar particle and x-ray fluxes. The experiments were designed to investigate physical processes occurring at the magnetopause and the mechanisms of particle acceleration. This spacecraft malfunctioned from the first day of launch due to commutator and power system problems. A very limited amount of useful data was obtained. The satellite became inoperable as of October 1972.

1 Payload

13 kilograms

OV5-5

Wiki

The satellite had an octagonal configuration, was spin-stabilized, and was placed in a moderately elliptical earth orbit (eccentricity - 0.670) by a Titan 3C on May 25, 1969. The purpose of the satellite was to monitor x-ray, electron, and proton radiation associated with solar activity in order to develop data handling techniques in near real-time for use by the Air Weather Service Forecast Center in forecasting solar flares.

1 Payload

11 kilograms

Rocket

Retired
Titan IIIC

Active 1965 to 1970

United States Air Force logo

Manufacturer

US Air Force

Rocket

Height: 42m

Payload to Orbit

LEO: 13,100 kg

GTO: 3,000 kg

Liftoff Thrust

13,642 Kilonewtons

Fairing

Diameter: 3m

Stages

3

Strap-ons

2

Launch Site

SLC-41

Cape Canaveral SFS, Florida, USA

Fastest Turnaround

15 days 22 hours

Stats

Titan III


38th

Mission

5th

Mission of 1969

1969


53rd

Orbital launch attempt