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: | |
| Equipment: | |
| Configuration: | |
| Propulsion: | none |
| Lifetime: | |
| Mass: | 10 kg |
| Orbit: | 559 km x 3320 km, 32.88° |
| Satellite | Date | LS | Launcher | Remarks: | |
|---|---|---|---|---|---|
| Vanguard SLV3 (20in Cloud cover #1) | 26.09.1958 | CC LC-18A | F | Vanguard | |
| Vanguard 2 (20in Cloud cover #2) | 17.02.1959 | CC LC-18A | Vanguard |
| Further Vanguard missions: |
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs