Soyuz 11A514
Launch vehicle · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: © Mark Wade
Russian orbital launch vehicle. Version of Soyuz launcher with increased payload, designed to launch Soyuz R military reconnaissance satellite. Cancelled along with the Soyuz R project in 1966. Unknown differences to standard Soyuz to reach payload requirement of circa 6700 kg to 65 degree orbit.
LEO Payload: 6,700 kg (14,700 lb) to a 200 km orbit at 65.00 degrees.
Related
- Family
- orbital launch vehicle
- Country
- Russia
- Spacecraft
- Soyuz VI
- Agency
- Korolev bureau