Miranda (X-4)

Launch Success

Liftoff Time (GMT)

02:22:00

Saturday March 9, 1974

Mission Details

Miranda (X-4)

Wiki

The British Miranda satellite, also known as X-4, was an experimental spacecraft. It was designed to serve as an engineering test bed to check the application of a three-axis integrating gyro system for attitude control and a three-axis rate gyro system for rate control. The satellite was in the form of a box 83.5 cm high, with a square base 66.5 cm on a side. Electrical power to the spacecraft was supplied from batteries and solar panels. When fully deployed the panels measured 250 cm in length.

Polar Orbit

1 Payload

92 kilograms

Rocket

Retired
Scout D1

Active 1972 to 1979

Vought logo

Manufacturer

Vought

Rocket

Height: 21m

Payload to Orbit

LEO: 185 kg

GTO: 0 kg

Liftoff Thrust

622 Kilonewtons

Stages

4

Launch Site

SLC-5

Vandenberg SFB, California, USA

Fastest Turnaround

11 days 17 hours

Stats

Scout


68th

Mission

2nd

Mission of 1974

1974


14th

Orbital launch attempt