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Angara 1.1
Part of Angara
Angara 1.1
Angara 1.1
Credit: © Mark Wade
Russian orbital launch vehicle. The initial flight version would be the Angara 1.1, featuring a single URM core module with the existing Briz upper stage. Payload would be 2.0 metric tons to a 200 km / 63 deg orbit). Other vehicle variants were numbered according to the number of URM's.

Status: In development. Payload: 2,000 kg (4,400 lb). Thrust: 1,910.00 kN (429,380 lbf). Gross mass: 145,000 kg (319,000 lb). Height: 34.90 m (114.50 ft). Diameter: 3.90 m (12.70 ft). Apogee: 200 km (120 mi).

LEO Payload: 2,000 kg (4,400 lb) to a 200 km orbit at 63.00 degrees.

Stage Data - Angara 1.1



Family: orbital launch vehicle. Country: Russia. Stages: Angara UM, Angara Briz M stage. Agency: Chelomei bureau.
Photo Gallery

Angara LV FamilyAngara LV Family
Credit: © Mark Wade


Briz MBriz M
Credit: Khrunichev


AngaraAngara
Credit: © Mark Wade


Angara KhrunichevAngara Khrunichev
Angara Khrunichev model
Credit: Khrunichev



1994 August 30 - . LV Family: Angara. Launch Vehicle: Angara 1.1.
1999 June 12 - . LV Family: Angara. Launch Vehicle: Angara 1.1.

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