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 France
Manufactured in France
Manufactured in France
Manufactured in France
Manufactured in France
Manufactured in France
Manufactured in France
Manufactured in France
Manufactured in France
| 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 | FRA | Aérospatiale Aerospace | Aestus | - | NTO-MMH | Liquid | Liquid | 1 | 1,000 | 0.43 | 3.96 | 83 : 1 | 2,700.00 | 27.40 | 1.03 | 24.87 | 0.94 | |
| 2 | FRA | Aérospatiale Aerospace | HM7-A | - | LOx-Hydrogen | Liquid | Liquid | 1 | 3,000 | 0.12 | 0.93 | 62.5 : 1 | 149.00 | 61.70 | 42.22 | 42.50 | 29.08 | |
| 3 | FRA | Aérospatiale Aerospace | HM7-B | - | LOx-Hydrogen | Liquid | Liquid | 1 | 3,500 | 0.11 | 1.00 | 83.1 : 1 | 155.00 | 70.00 | 46.05 | 43.60 | 28.68 | |
| 4 | FRA | Aérospatiale Aerospace | Mage-1 | - | AP-HTPB-Al | Solid | Solid | 1 | 4,900 | 0.11 | 0.77 | 45 : 1 | 34.00 | 19.40 | 58.18 | 14.50 | 43.49 | |
| 5 | FRA | Aérospatiale Aerospace | Mage-2 | - | AP-HTPB-Al | Solid | Solid | 1 | 4,800 | 0.10 | 0.77 | 65 : 1 | 40.00 | 45.50 | 115.99 | 34.01 | 86.69 | |
| 6 | FRA | Aérospatiale Aerospace | Viking-2 | - | NTO-UDMH | Liquid | Liquid | 1 | 5,500 | 0.29 | 0.95 | 11 : 1 | 776.00 | 693.00 | 91.06 | 611.62 | 80.37 | |
| 7 | FRA | Aérospatiale Aerospace | Viking-2B | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,900 | 0.29 | 0.95 | 11 : 1 | 776.00 | 720.00 | 94.61 | 642.30 | 84.40 | |
| 8 | FRA | Aérospatiale Aerospace | Viking-4 | - | NTO-UDMH | Liquid | Liquid | 1 | 5,400 | 0.47 | 2.60 | 31 : 1 | 826.00 | 720.97 | 89.00 | 485.50 | 59.93 | |
| 9 | FRA | Aérospatiale Aerospace | Viking-4B | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,850 | 0.47 | 2.60 | 30.8 : 1 | 826.00 | 805.00 | 99.38 | 571.11 | 70.50 | |
| 10 | FRA | Aérospatiale Aerospace | Viking-5C | - | NTO-Aerozine-25 | Liquid | Liquid | 1 | 5,500 | 0.67 | 2.22 | 11 : 1 | 826.00 | 752.00 | 92.83 | 670.85 | 82.81 | |
| 11 | FRA | Aérospatiale Aerospace | Viking-6 | - | NTO-Aerozine-25 | Liquid | Liquid | 4 | 5,500 | 0.67 | 2.22 | 11 : 1 | 826.00 | 752.00 | 92.83 | 670.80 | 82.81 | |
| 12 | FRA | Aérospatiale Aerospace | Vulcain | - | LOx-Hydrogen | Liquid | Liquid | 1 | 10,888 | 0.81 | 5.46 | 45 : 1 | 12,700.00 | 1,114.00 | 8.94 | 993.71 | 7.98 | |
| 13 | FRA | Aérospatiale Aerospace | Vulcain-2 | - | LOx-Hydrogen | Liquid | Liquid | 1 | 10,888 | 0.81 | 5.46 | 45 : 1 | 12,700.00 | 1,114.00 | 8.94 | 993.71 | 7.98 | |
| 14 | FRA | Aérospatiale Aerospace | Zefiro-9 | - | AP-HTPB-Al | Solid | Solid | 1 | 7,400 | 0.25 | 1.90 | 56 : 1 | 1,315.00 | 313.00 | 24.27 | 260.00 | 20.16 | |
| 15 | FRA | Aérospatiale Aerospace | Zefiro-23 | - | AP-HTPB-Al | Solid | Solid | 1 | 10,600 | 0.38 | 1.90 | 25 : 1 | 2,850.00 | 871.00 | 31.16 | 781.37 | 27.96 | |
| 16 | FRA | Safran Aircraft Engines | Astris | - | NTO-Aerozine-50 | Liquid | Liquid | 1 | 3,100 | 0.32 | 2.00 | 40 : 1 | 68.00 | 23.60 | 35.39 | 19.60 | 29.39 | |
| 17 | FRA | SEREB | P6 | - | AP-HTPB-Al | Solid | Solid | 1 | 3,000 | 0.23 | 1.50 | 42.75 : 1 | 120.00 | 36.19 | 30.75 | 29.40 | 24.98 | |
| 18 | FRA | SEREB | Topaze | - | NTO-UDMH | Liquid | Liquid | 1 | 3,000 | 0.12 | 0.80 | 42.75 : 1 | 540.00 | 120.08 | 22.68 | 105.75 | 19.97 | |
| 19 | FRA | SEREB | Vexin-A | - | NTO-UDMH | Liquid | Liquid | 1 | 3,000 | 0.08 | 0.50 | 42.75 : 1 | 175.00 | 68.60 | 39.97 | 59.50 | 34.67 | |
| 20 | FRA | SEREB | Vexin-B | - | NTO-UDMH | Liquid | Liquid | 1 | 3,000 | 0.05 | 0.34 | 42.75 : 1 | 192.00 | 75.40 | 40.04 | 66.40 | 35.26 | |
| 21 | FRA | SEREB | Vexin-C | - | NTO-UDMH | Liquid | Liquid | 1 | 3,000 | 0.05 | 0.34 | 42.75 : 1 | 252.00 | 99.10 | 40.10 | 87.30 | 35.32 | |
| 22 | FRA | SNPE | P7.35 | - | AP-HTPB-Al | Solid | Solid | 1 | 3,000 | 0.16 | 1.07 | 42.75 : 1 | 2,313.00 | 690.00 | 30.42 | 629.60 | 27.76 | |
| 23 | FRA | SNPE | P9.5 | - | AP-HTPB-Al | Solid | Solid | 1 | 3,000 | 0.16 | 1.07 | 42.75 : 1 | 3,060.00 | 690.00 | 22.99 | 629.60 | 20.98 | |
| 24 | FRA | SNPE | P230 | - | AP-HTPB-Al | Solid | Solid | 1 | 6,130 | 0.98 | 3.05 | 9.7 : 1 | 19,900.00 | 3,236.15 | 16.58 | 2,952.87 | 15.13 | |
| 25 | FRA | SNPE | P238 | - | AP-HTPB-Al | Solid | Solid | 1 | 6,130 | 0.98 | 3.05 | 9.7 : 1 | 19,900.00 | 3,236.15 | 16.58 | 2,952.87 | 15.13 | |
| 26 | FRA | SNPE | P241 | - | AP-HTPB-Al | Solid | Solid | 1 | 6,130 | 0.98 | 3.05 | 9.7 : 1 | 19,100.00 | 3,235.00 | 17.27 | 2,951.82 | 15.76 | |
| 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 |