Fregat

Fregat
Model of Fregat at MAKS Airshow, 2013
ManufacturerNPO Lavochkin
Country of originRussia
Used onCurrent: Soyuz-2
Retired: Soyuz-FG, Soyuz-ST, Soyuz-U, Zenit-3F
Launch history
StatusActive
Total launches114
Successes
(stage only)
111
Failed2
Other1 (partial failure)
First flight2 February 2000
General characteristics
HeightFregat: 1.875 m (6 ft 1.8 in)
Fregat-MT: 1.945 m (6 ft 4.6 in)
Fregat-SB: 2.435 m (7 ft 11.9 in)
DiameterFregat: 3.44 m (11.3 ft)
Fregat-MT: 3.8 m (12 ft)
Fregat-SB: 3.875 m (12.71 ft)
Empty massFregat: 945 kg (2,083 lb)
Fregat-MT: 1,035 kg (2,282 lb)
Fregat-SB: 1,080 kg (2,380 lb)
Gross massFregat: 6,235 kg (13,746 lb)
Fregat-MT: 7,640 kg (16,840 lb)
Fregat-SB: 11,680 kg (25,750 lb)
Propellant massFregat: 5,307 kg (11,700 lb)
Fregat-MT: 6,650 kg (14,660 lb)
Fregat-SB: 10,330 kg (22,770 lb)
Powered by1 × S5.92
Maximum thrust19.85 kN (4,460 lbf) (high)
13.93 kN (3,130 lbf) (low)
Specific impulse333.2 s (3.268 km/s) (high)
320 s (3.1 km/s) (low)
Burn timeUp to 1,350 seconds (up to 7 starts)
PropellantN2O4/UDMH

Fregat (Russian: Фрегат, lit.'frigate') is an upper stage developed by NPO Lavochkin for universal compatibility with a wide range of medium- and heavy-lift launch vehicles. Fregat has been used primarily with Soyuz and Zenit rockets, and entered operational service in February 2000.

Fregat uses a liquid-propellant engine burning unsymmetrical dimethylhydrazine (UDMH) fuel and dinitrogen tetroxide (N2O4) oxidizer, a pair of hypergolic propellants that ignite on contact. With a success rate of 97.3%, including two failures and one partial failure, Fregat is among the most reliable upper stages in operation. It has deployed more than 300 payloads into a variety of orbits and is capable of placing three or more spacecraft into distinct orbits during a single mission, owing to its ability to restart up to seven times and operate for a total burn duration of up to 1,350 seconds.