Chalet/Vortex
Chalet/Vortex was even larger than Rhyolite, weighing around 1800 kilograms and having a 38-meter diameter antenna. Its primary mission was to intercept communications carried on UHF radio links which used antennae directed towards stationary orbit, or antennae with wide main lobes. There were six launches in total: Chalet-1 (10 June 1978) and Vortex 1–5 (1 October 1979–10 May 1989). The second batch of three Vortex satellites, launched from 1984 to 1989, probably had enhanced sensors. One was stranded in the wrong orbit when its Titan Transstage (transfer stage) malfunctioned. Each Chalet/Vortex satellite had a nominal lifetime of 5 to 7 years.
launch vehicle | Titan-3C and -34D |
site | Cape Canaveral |
orbit | quasi-GSO 32,940 × 38,330 km × 5.5° |
size | 38.4 × 36.6 m |
mass | 1,800 kg |