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Function | Launch Vehicle |
---|---|
Manufacturer | AgniKul Cosmos |
Country of origin | India |
Size | |
Height | 18 m (59 ft) |
Diameter | 1.3 m (4 ft 3 in) |
Mass | 14,000 kg (31,000 lb) |
Stages | 2-3 |
Capacity | |
Payload to LEO | Altitude 700 km (430 mi)
Orbital inclination 45.0° Mass 100 kg (220 lb) |
Launch history | |
Status | Under Development |
First stage | |
Engines | 4/5/6/7 × Agnilet (Customizable) |
Thrust | 140 kN (sea level) |
Burn time | 285 sec |
Propellant | LOX/ RP-1 |
Second stage | |
Engines | 1 × Agnilet |
Thrust | 25 kN (sea level) |
Burn time | 355 sec |
Propellant | LOX / RP-1 |
Third stage | |
Engines | 1 × Agnilet |
Propellant | LOX / RP-1 |
Agnibaan (Sanskrit, ISO: Agni 'Fire', Bāṇa 'Arrow', lit. 'Arrow of Fire'), produced by Agnikul Cosmos in Chennai, India, is a mobile small-lift launch system currently under development. It is capable of placing a 100 kg (220 lb) satellite into a 700 km (430 mi) orbit. The rocket will be 18 meters long with a diameter of 1.3 meters and a lift-off mass of 14,000 kg (31,000 lb).[1][2][3][4] The Agnibaan rocket has three stages. The first stage is powered by seven Agnilet engines.[1] The second stage is powered by the same Agnilet engine which will have a larger nozzle than the sea level nozzle to optimize it for vacuum.[2]
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