SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
ROCKET ENGINE REGISTER
ROCKET ENGINE REGISTER
ROCKET ENGINE REGISTER
ROCKET ENGINE REGISTER
ROCKET ENGINE REGISTER
Manufactured in India
Manufactured in India
Manufactured in India
Manufactured in India
Manufactured in India
Manufactured in India
Manufactured in India
Manufactured in India
Manufactured in India
| ID | Country | Manufacturer | Engine | AKA | Propellant ID | Oxidiser | Fuel | Chambers | Chamber Pressure | Nozzle Diameter Initial | Nozzle Diameter Exit | Nozzle Expansion Ratio | Engine Weight | Vacuum Thrust | V Thrust Weight Ratio | Sea Level Thrust | SL Thrust Weight Ratio | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 1 | IND | Hindustan Aeronautics | CE20 | - | LOx-Hydrogen | Liquid | Liquid | 1 | 5,300 | 1.07 | 4.00 | 13.9 : 1 | 588.00 | 200.00 | 34.68 | 172.27 | 29.87 | |
| 2 | IND | Hindustan Aeronautics | CLPS | - | Hydrazine | Mono | - | 1 | 4,200 | 0.17 | 1.20 | 52 : 1 | 180.00 | 0.41 | 0.23 | 0.35 | 0.20 | |
| 3 | IND | Hindustan Aeronautics | CLPS+ | - | Hydrazine | Mono | - | 1 | 4,200 | 0.17 | 1.20 | 52 : 1 | 155.00 | 0.41 | 0.27 | 0.35 | 0.23 | |
| 4 | IND | ISRO | HTVE-1 | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,300 | 0.38 | 1.40 | 13.9 : 1 | 4,400.00 | 680.50 | 15.77 | 600.50 | 13.92 | |
| 5 | IND | ISRO | HTVE-2 | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,300 | 0.48 | 1.80 | 13.9 : 1 | 5,550.00 | 846.80 | 15.56 | 757.10 | 13.91 | |
| 6 | IND | ISRO | HTVE-2-2 | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,300 | 0.48 | 1.80 | 13.9 : 1 | 11,100.00 | 1,693.60 | 15.56 | 1,514.20 | 13.91 | |
| 7 | IND | ISRO | I-SLV-1 | - | AP-HTPB-Al | Solid | Solid | 1 | 4,300 | 0.39 | 1.00 | 6.7 : 1 | 335.00 | 83.77 | 25.50 | 73.66 | 22.42 | |
| 8 | IND | ISRO | I-SLV-2 | - | AP-HTPB-Al | Solid | Solid | 1 | 4,300 | 0.21 | 0.80 | 14 : 1 | 1,750.00 | 267.00 | 15.56 | 216.00 | 12.59 | |
| 9 | IND | ISRO | I-SLV-3 | - | AP-HTPB-Al | Solid | Solid | 1 | 4,300 | 0.17 | 0.82 | 24 : 1 | 440.00 | 90.70 | 21.02 | 62.20 | 14.41 | |
| 10 | IND | ISRO | I-SLV-4 | - | AP-HTPB-Al | Solid | Solid | 1 | 2,900 | 0.12 | 0.66 | 31 : 1 | 98.00 | 26.80 | 27.89 | 25.69 | 26.73 | |
| 11 | IND | ISRO | PSLV-1 | - | AP-HTPB-Al | Solid | Solid | 1 | 5,800 | 0.99 | 2.80 | 8 : 1 | 31,200.00 | 4,860.00 | 15.88 | 4,363.00 | 14.26 | |
| 12 | IND | ISRO | PSLV-2 | - | AP-HTPB-Al | Solid | Solid | 1 | 4,300 | 0.75 | 2.80 | 14 : 1 | 5,300.00 | 725.02 | 13.95 | 650.88 | 12.52 | |
| 13 | IND | ISRO | PSLV-3 | - | AP-HTPB-Al | Solid | Solid | 1 | 4,300 | 0.41 | 1.99 | 24 : 1 | 1,100.00 | 328.71 | 30.47 | 295.09 | 27.35 | |
| 14 | IND | ISRO | PSLV-4 | - | AP-HTPB-Al | Solid | Solid | 1 | 840 | 0.17 | 1.34 | 60 : 1 | 460.00 | 7.00 | 1.55 | 6.28 | 1.39 | |
| 15 | IND | ISRO | S200 | - | AP-HTPB-Al | Solid | Solid | 1 | 5,692 | 0.94 | 3.27 | 12.1 : 1 | 15,650.00 | 6,228.85 | 40.58 | 5,151.00 | 33.56 | |
| 16 | IND | ISRO | Vikas-1 | - | NTO-UDMH | Liquid | Liquid | 1 | 5,300 | 0.27 | 1.00 | 13.9 : 1 | 800.00 | 680.50 | 86.74 | 600.50 | 76.54 | |
| 17 | IND | ISRO | Vikas-1+ | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,300 | 0.27 | 1.00 | 13.9 : 1 | 900.00 | 765.50 | 86.73 | 677.70 | 76.78 | |
| 18 | IND | ISRO | Vikas-2 | - | NTO-UDMH | Liquid | Liquid | 1 | 5,300 | 0.46 | 1.70 | 13.9 : 1 | 850.00 | 725.00 | 86.97 | 640.00 | 76.78 | |
| 19 | IND | ISRO | Vikas-2B | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,850 | 0.46 | 1.70 | 13.9 : 1 | 900.00 | 765.50 | 86.73 | 677.70 | 76.78 | |
| 20 | IND | ISRO | Vikas-X | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,300 | 0.48 | 1.80 | 13.9 : 1 | 980.00 | 839.00 | 87.30 | 756.50 | 78.71 | |
| 21 | IND | ISRO | Vikas-4 | - | NTO-UDMH | Liquid | Liquid | 1 | 5,300 | 0.40 | 1.50 | 13.9 : 1 | 850.00 | 725.00 | 86.97 | 653.71 | 78.42 | |
| 22 | IND | ISRO | Vikas-4B | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,850 | 0.48 | 1.80 | 13.9 : 1 | 940.00 | 804.00 | 87.22 | 724.94 | 78.64 | |
| ID | Country | Manufacturer | Engine | AKA | Propellant ID | Oxidiser | Fuel | Chambers | Chamber Pressure | Nozzle Diameter Initial | Nozzle Diameter Exit | Nozzle Expansion Ratio | Engine Weight | Vacuum Thrust | V Thrust Weight Ratio | Sea Level Thrust | SL Thrust Weight Ratio |