Ariane Passenger Payload Experiment
| Mission type | Communications |
|---|---|
| Operator | EADS Astrium |
| COSPAR ID | 1981-057B |
| SATCAT no. | 12545 |
| Mission duration | 2 years, 3 months |
| Spacecraft properties | |
| Manufacturer | ISRO |
| Launch mass | 350 kilograms (770 lb) |
| Start of mission | |
| Launch date | 19 June 1981 |
| Rocket | Ariane 1 |
| Launch site | Kourou ELA-1 |
| End of mission | |
| Deactivated | 19 September 1983 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Geostationary |
| Longitude | 102° East |
The Ariane Passenger PayLoad Experiment (APPLE), was an experimental communication satellite with a C-Band transponder launched by the Indian Space Research Organisation on June 19, 1981, by Ariane, a launch vehicle of the European Space Agency (ESA) from Centre Spatial Guyanais near Kourou in French Guiana.
APPLE was India's first three-axis stabilised experimental Geostationary communication satellite. On July 16, 1981, the satellite was positioned at 102° E longitude. The 672 kg satellite served as testbed of the Indian telecommunications space relay infrastructure despite the failure of one solar panel to deploy. Solid-propellant based Apogee Boost Motor to circularize APPLE's orbit was derived from SLV-3 fourth stage.
It was used in several communication experiments including relay of TV programmes and radio networking. It was a cylindrical spacecraft measuring 1.2 m in diameter and 1.2 m high. Its payload consisted of two 6/4 GHz transponders connected to a 0.9 m diameter parabolic antenna. It went out of service on September 19, 1983. R. M. Vasagam was the project director of APPLE during 1977-1983.
| Mission | Experimental geostationary communication |
| Weight | 670 kg |
| Onboard Power | 210 watts |
| Payload | C-band transponders (Two) |
| Launch Date | June 19, 1981 |
| Launch Vehicle | Ariane -1(V-3) |
| Orbit | Geosynchronous |
| Mission life | Two years |