Function | Medium to Heavy-lift launch vehicle |
---|---|
Manufacturer | ISRO |
Country of origin | India |
Size | |
Height | 93 m (305 ft)[1] |
Width | 5 m (16 ft) |
Mass | 600 t (590 long tons; 660 short tons) to 1,094 t (1,077 long tons; 1,206 short tons) |
Booster stage – S200 Boosters (NGLV-H) | |
Height | 25 m (82 ft)[2] |
Diameter | 3.2 m (10 ft)[3] |
Empty mass | 31,000 kg (68,000 lb) each[4] |
Gross mass | 236,000 kg (520,000 lb) each[4] |
Propellant mass | 205,000 kg (452,000 lb) each[4] |
Powered by | Solid S200 |
Maximum thrust | 5,151 kN (525.3 tf)[5][6] |
Specific impulse | 274.5 seconds (2.692 km/s) (vacuum)[4] |
Burn time | 128 s[4] |
Propellant | HTPB / AP[4] |
First stage – (NGLV/NGLV-H) | |
Diameter | 5.0 m (16.4 ft) |
Powered by | 9 LME-110 |
Propellant | LOX / CH4 |
Second stage – (NGLV/NGLV-H) | |
Diameter | 5.0 m (16.4 ft) |
Powered by | 2 LME-110 |
Propellant | LOX / CH4 |
Third stage – C32 (NGLV/NGLV-H) | |
Diameter | 5.0 m (16.4 ft)[4] |
Propellant mass | 32,000 kg (71,000 lb)[4] |
Powered by | 1 CE-20[U] |
Maximum thrust | 216 kN (22.0 tf)[4] |
Specific impulse | 443 seconds (4.34 km/s) |
Propellant | LOX / LH2 |
Stages | 3 |
Capacity | |
Payload to LEO | |
Mass | 30–70 t (66,000–154,000 lb)[7] |
Payload to GTO | |
Mass | 8,500 to 24,000 kg (18,700 to 52,900 lb)[citation needed] |
Payload to TLI | |
Mass | 7,000 to 22,500 kg (15,400 to 49,600 lb)[citation needed] |
Associated rockets | |
Comparable | |
Launch history | |
Status | Under Development |
Launch sites | Satish Dhawan TLP |
First flight | 2031
|
Type of passengers/cargo | [8] |
The Next Generation Launch Vehicle (NGLV)(Soorya-:unofficial name) is a three-stage partially reusable Heavy-lift launch vehicle, currently under development by the Indian Space Research Organisation (ISRO). This vehicle is designed to replace currently operational systems like PSLV, GSLV and LVM3. The project was previously referred to as Unified Launch Vehicle (ULV).[9][10][11]
This family of three launchers was previously being designed for replacing the different core propulsion modules of PSLV, GSLV, and LVM3 respectively with a common semi-cryogenic engine and hence it was named as Unified Launch Vehicle (ULV).[12] Unlike the latest proposal of the launcher, the initial proposals were planned to be expendable. But the new proposals under the name of Next Generation Launch Vehicle (NGLV) suggests launchers having partial reusability.[13]
S. Sivakumar is the program director for ISRO's Space Transportation System and the projector director for NGLV at Vikram Sarabhai Space Centre (VSSC).[14][15]