Cosmos 1460

Launch Success

Liftoff Time (GMT)

09:10:00

Friday May 6, 1983

Mission Details

Cosmos 1460

Wiki

Zenit was a series of military photoreconnaissance satellites launched by the Soviet Union between 1961 and 1994. The basic design of the Zenit satellites was similar to the Vostok crewed spacecraft, sharing the return and service modules. It consisted of a spherical re-entry capsule 2.3 metres in diameter with a mass of around 2,400 kilograms. This capsule contained the camera system, its film, recovery beacons, parachutes and a destruct charge. In orbit, this was attached to a service module that contained batteries, electronic equipment, an orientation system and a liquid fuelled rocket engine that would slow the Zenit for re-entry, before the service module detached. The total length in orbit was around 5 metres. Unlike the American Corona spacecraft, the return capsule carried both the film and the cameras and kept them in a temperature controlled pressurised environment. This simplified the design and engineering of the camera system but added considerably to the mass of the satellite. An advantage was that cameras could be reused. Most Zenits flew in a slightly elliptical orbit with a perigee of around 200 kilometres (120 miles) and an apogee between 250 and 350 kilometres (160 and 220 miles); the missions usually lasted between 8 and 15 days.

Low Earth Orbit

1 Payload

6,300 kilograms

Rocket

Retired
Soyuz U

Active 1973 to 2017

RKK Energiya logo

Manufacturer

RKK Energiya

Price

$20.00 million

Rocket

Height: 51.32m

Payload to Orbit

LEO: 6,860 kg

GTO: 0 kg

Liftoff Thrust

4,456 Kilonewtons

Fairing

Diameter: 3m

Height: 15.59m

Stages

3

Strap-ons

4

Launch Site

Site 31/6

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

47 hr 9 min

Stats

Soyuz U


323rd

Mission

13th

Mission of 1983

RKK Energiya


1704th

Mission

35th

Mission of 1983

1983


44th

Orbital launch attempt