Kondor-FKA No.2

The mission

The Kondor-FKA is a small civilian radar Earth observation satellite designed by NPO Mashinostroyeniya as a civilian counterpart to the Kondor-E satellite. The Kondor satellite features a S-band synthetic aperture radar (SAR), which can conduct both continous swath surweys or detailed spot surveys. The swath width is 10 km. Ground resolution is 1 to 2 m in spotlight mode, 1 to 3 m in stripmap mode and 5 to 30 m in ScanSAR mode.

Type

Earth science

Destination

Sun-synchronous orbit

The rocket

The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle.

The operator

Russian Federal Space Agency (ROSCOSMOS)

The Roscosmos State Corporation for Space Activities, commonly known as Roscosmos, is the governmental body responsible for the space science program of the Russian Federation and general aerospace research. Soyuz has many launch locations the Russian sites are Baikonur, Plesetsk and Vostochny however Ariane also purchases the vehicle and launches it from French Guiana.

Sector

Government

Based in

Russia

Founded

1992

Run by

Yuri Borisov, Administrator

343 launches so far, 332 of them successful. The last 67 in a row went to plan.

en.roscosmos.ru → Wikipedia →

The launch site

It went up from Cosmodrome Site 1S at Vostochny Cosmodrome, Siberia, Russia.

See the pad on a map →