ULV
Country of Origin: India
Manufacturer: LPSC, ISRO
Height:
Diameter:
Payload to LEO: 270 – 700 tons
Total Mass: 4.5 to 15 tons
Launch Sites:
First Flight: In development
Last Flight:
Total Launches:
Successful Launches:
ULV
| Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
|---|---|---|---|---|---|---|---|
| Booster Option 1 | 1 m | HTPB | 6 x S-13 | 70 s (?) | 6 x 716 kN | Prop mass: 12.2 tons each | |
| Booster Option 2 | HTPB | 2 x S-60 | Prop mass: 60 tons each | ||||
| Booster Option 3 | 2.8 m | HTPB | 2 x S-139 | 100 s | 2 x 4700 kN | Prop mass: 138.2 tons each | |
| Booster Option 4 | 3.2 m | HTPB | 2 x S-200 | 130 s | 2 x 5150 kN | ? / 274.5 s | Prop mass: 207 tons each |
| 1 (SC-160) | RP-1 / LOX | SCE-200 | 259 s | 2030 kN | 299 s / 335 s | Prop mass: 160 tons | |
| 2 (C-30) | LH2 / LOX | CE-20 | 650 s | 200 kN | ? / 443 s | Prop mass: 30 tons |
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