The Soyuz-2-1v (formerly called Soyuz-1) is a lightweight derivative of the Soyuz launch vehicle. It ommits the four strap-on boosters and features a modified core. While originally the core with a NK-33-1 engine was planned, the core had to modified to a larger diameter, when the development of the NK-33-1 was cancelled and replaced with a NK-33A and an additional RD-0110 vernier engine.
The first flight is planned for 2012 from Plesetsk.
|Version||Stage 1||Stage 2|
|Soyuz-2-1v (Soyuz-1)||Blok-A / NK-33A + RD-0110R||Blok-I mod. / RD-0124|
Nr TNr Vehicle Serial Date Sc LS Payload
None planned: Launch sites: Pl = Plesetsk (NIIP-53, GIK-1, GNIIP), Russia Vo = Vostochniy, Amurskaya Oblast', Russia