Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

Vanguard (20in Cloud Cover)

Vanguard 2 [NASA]

Vanguard SLV-3 and Vanguard 2 were earth-orbiting satellites designed to measure cloud-cover distribution over the daylight portion of its orbit. The spacecraft was a magnesium sphere 50.8 cm in diameter. It contained two optical telescopes with two photocells. The sphere was internally gold-plated and externally covered with an aluminum deposit coated with silicon oxide of sufficient thickness to provide thermal control for the instrumentation. Radio communication was provided by a 1 W, 108.03 MHz telemetry transmitter and a 10 mW, 108 MHz beacon transmitter that sent a continuous signal for tracking purposes. A command receiver was used to activate a tape recorder that relayed telescope experiment data to the telemetry transmitter. Both transmitters functioned normally for 19 days. The satellite was spin stabilized at 50 rpm, but telemetry data were poor because of an unsatisfactory orientation of the spin axis. The power supply for the instrumentation was provided by mercury batteries.

Nation: USA
Type / Application: Science
Operator: NASA
Contractors: Naval Research Laboratory (NRL)
Propulsion: None
Power: Batteries
Mass: 10 kg
Orbit: 559 km × 3320 km, 32.88
Satellite COSPAR Date LS Launch Vehicle Remarks
Vanguard SLV3 (20in Cloud cover #1) 1958-F16 26.09.1958 CC LC-18A F Vanguard
Vanguard 2 (20in Cloud cover #2) 1959 α 1 17.02.1959 CC LC-18A Vanguard