| Mission type | OSCAR | 
|---|---|
| Operator | University of Surrey | 
| COSPAR ID | 1981-100B | 
| SATCAT no. | 12888 | 
| Spacecraft properties | |
| Launch mass | 54 kilograms (119 lb) | 
| Start of mission | |
| Launch date | 6 October 1981, 11:27 UTC | 
| Rocket | Delta 2310 D-157 | 
| Launch site | Vandenberg SLC-2W | 
| Orbital parameters | |
| Reference system | Geocentric | 
| Regime | Low Earth | 
| Perigee altitude | 372 kilometres (231 mi) | 
| Apogee altitude | 374 kilometres (232 mi) | 
| Inclination | 97.6° | 
| Period | 92 minutes | 
UoSAT-1, also known as UoSAT-OSCAR 9 (UO-9), was a British amateur radio satellite which orbited Earth. It was built at the University of Surrey and launched into low Earth orbit on 6 October 1981. It exceeded its anticipated two-year orbital lifespan [1] by six years, having received signals on 13 October 1989, [2] before re-entering the atmosphere.
This was the first of several UoSAT satellites; followed by UoSAT-2.
Like its successor UoSAT-2 it carried a CCD camera and a Digitalker speech synthesiser, [1] and transmitted telemetry data on a 145.826 MHz beacon at 1200 baud using asynchronous AFSK. [3]
The Astrid package sold by British firm MM Microwave, [4] consisting of a fixed frequency VHF receiver set and software for the BBC Micro, could display the telemetry frames from either UoSAT-1 or UoSAT-2. [1] UoSAT-1's solar arrays were of an experimental design reused for UoSAT-2. [1]
The primary computer for the satellite was the RCA 1802 microprocessor. [5] A secondary microprocessor was also employed, the "F100L" (a Ferranti 16-bit processor). Memory was 16K of DRAM.