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
LAUNCH VEHICLE REGISTER
LAUNCH VEHICLE REGISTER
LAUNCH VEHICLE REGISTER
LAUNCH VEHICLE REGISTER
LAUNCH VEHICLE REGISTER
Manufactured in North Korea
Manufactured in North Korea
Manufactured in North Korea
Manufactured in North Korea
Manufactured in North Korea
Manufactured in North Korea
Manufactured in North Korea
Manufactured in North Korea
Manufactured in North Korea
| ID | Country | Family | Vehicle | AKA | Stages | Total Length | LEO Payload | MEO Payload | GEO Payload | Stage 0 | 0 Length | 0 Engine | 0 Quantity | 0 Propellant ID | 0 Propellant Ox | 0 Propellant Fuel | 0 Burn Rate | 0 Flow Rate | 0 Empty | 0 Propellant | 0 Gross | 0 Upper | 0 Net | 0 VAC Thrust | 0 VAC Specific Impulse | 0 VAC T-W Ratio | 0 SL Thrust | 0 SL Specific Impulse | 0 SL T-W Ratio | Stage 1 | 1 Length | 1 Engine | 1 Quantity | 1 Propellant ID | 1 Propellant Ox | 1 Propellant Fuel | 1 Burn Rate | 1 Flow Rate | 1 Empty | 1 Propellant | 1 Gross | 1 Upper | 1 Net | 1 VAC Thrust | 1 VAC Specific Impulse | 1 VAC T-W Ratio | 1 SL Thrust | 1 SL Specific Impulse | 1 SL T-W Ratio | Stage 2 | 2 Length | 2 Engine | 2 Quantity | 2 Propellant ID | 2 Propellant Ox | 2 Propellant Fuel | 2 Burn Rate | 2 Flow Rate | 2 Empty | 2 Propellant | 2 Gross | 2 Upper | 2 Net | 2 VAC Thrust | 2 VAC Specific Impulse | 2 VAC T-W Ratio | 2 SL Thrust | 2 SL Specific Impulse | 2 SL T-W Ratio | Stage 3 | 3 Length | 3 Engine | 3 Quantity | 3 Propellant ID | 3 Propellant Ox | 3 Propellant Fuel | 3 Burn Rate | 3 Flow Rate | 3 Empty | 3 Propellant | 3 Gross | 3 Upper | 3 Net | 3 VAC Thrust | 3 VAC Specific Impulse | 3 VAC T-W Ratio | 3 SL Thrust | 3 SL Specific Impulse | 3 SL T-W Ratio | Stage 4 | 4 Length | 4 Engine | 4 Quantity | 4 Propellant ID | 4 Propellant Ox | 4 Propellant Fuel | 4 Burn Rate | 4 Flow Rate | 4 Empty | 4 Propellant | 4 Gross | 4 Upper | 4 Net | 4 VAC Thrust | 4 VAC Specific Impulse | 4 VAC T-W Ratio | 4 SL Thrust | 4 SL Specific Impulse | 4 SL T-W Ratio | Stage 5 | 5 Length | 5 Engine | 5 Quantity | 5 Propellant ID | 5 Propellant Ox | 5 Propellant Fuel | 5 Burn Rate | 5 Flow Rate | 5 Empty | 5 Propellant | 5 Gross | 5 VAC Thrust | 5 VAC Specific Impulse | 5 VAC T-W Ratio | 5 SL Thrust | 5 SL Specific Impulse | 5 SL T-W Ratio | |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 1 | PRK | NADONG | Pekdosan-1 | - | 3 | 25.80 | 30.00 | - | - | 33,406 | 33,406 | Pekdosan-1 (1) | 12.00 | Nodong | 4 | RFNA-UDMH | Liquid | Liquid | 95.00 | 230.69 | 3,733 | 21,916 | 25,649 | 7,757 | 33,406 | 577.34 | 255.19 | 15.77 | 515.48 | 227.85 | 14.08 | Pekdosan-1 (2) | 12.00 | Nodong | 1 | RFNA-UDMH | Liquid | Liquid | 110.00 | 54.99 | 1,456 | 6,049 | 7,505 | 252 | 7,757 | 144.33 | 267.64 | 15.77 | 128.87 | 238.97 | 14.08 | Pekdosan-1 (3) | 1.80 | Hwasong | 1 | AP-HTPB-Al | Solid | Solid | 27.00 | 7.48 | 50 | 202 | 252 | 252 | 18.33 | 249.84 | 37.38 | 16.12 | 219.71 | 32.87 | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| 2 | PRK | UNHA | Unha-1 | - | 1 | 15.00 | - | - | - | 65,900 | 65,900 | Unha-1 (1) | 15.00 | Nodong-2-1 | 4 | RFNA-UDMH | Liquid | Liquid | 120.00 | 500.00 | 5,900 | 60,000 | 65,900 | 65,900 | 1,230.15 | 250.88 | 21.26 | 1,098.35 | 224.00 | 18.98 | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| 3 | PRK | UNHA | Unha-2 | - | 3 | 27.50 | 100.00 | - | - | 78,000 | 78,000 | Unha-2 (1) | 15.00 | Nodong-2-1 | 4 | RFNA-UDMH | Liquid | Liquid | 120.00 | 500.00 | 5,900 | 60,000 | 65,900 | 12,100 | 78,000 | 1,230.15 | 250.88 | 21.26 | 1,098.35 | 224.00 | 18.98 | Unha-2 (2) | 8.80 | Unha-B | 1 | RFNA-UDMH | Liquid | Liquid | 110.00 | 81.82 | 2,100 | 9,000 | 11,100 | 1,000 | 12,100 | 205.94 | 256.67 | 10.00 | 181.71 | 226.47 | 8.82 | Unha-2 (3) | 3.70 | Unha-C | 1 | RFNA-UDMH | Liquid | Liquid | 40.00 | 20.00 | 200 | 800 | 1,000 | 1,000 | 52.96 | 270.00 | 27.00 | 47.07 | 240.00 | 24.00 | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| 4 | PRK | UNHA | Unha-3 | - | 3 | 27.50 | 200.00 | - | - | 78,000 | 78,000 | Unha-3 (1) | 15.00 | Nodong-2-1 | 4 | RFNA-UDMH | Liquid | Liquid | 120.00 | 500.00 | 5,900 | 60,000 | 65,900 | 12,100 | 78,000 | 1,230.15 | 250.88 | 21.26 | 1,098.35 | 224.00 | 18.98 | Unha-3 (2) | 8.80 | Unha-B | 1 | RFNA-UDMH | Liquid | Liquid | 110.00 | 81.82 | 2,100 | 9,000 | 11,100 | 1,000 | 12,100 | 205.94 | 256.67 | 10.00 | 181.71 | 226.47 | 8.82 | Unha-3 (3) | 3.70 | Unha-C | 1 | RFNA-UDMH | Liquid | Liquid | 40.00 | 20.00 | 200 | 800 | 1,000 | 1,000 | 52.96 | 270.00 | 27.00 | 47.07 | 240.00 | 24.00 | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| 250.88 | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| ID | Country | Family | Vehicle | AKA | Stages | Total Length | LEO Payload | MEO Payload | GEO Payload | Stage 0 | 0 Length | 0 Engine | 0 Quantity | 0 Propellant ID | 0 Propellant Ox | 0 Propellant Fuel | 0 Burn Rate | 0 Flow Rate | 0 Empty | 0 Propellant | 0 Gross | 0 Upper | 0 Net | 0 VAC Thrust | 0 VAC Specific Impulse | 0 VAC T-W Ratio | 0 SL Thrust | 0 SL Specific Impulse | 0 SL T-W Ratio | Stage 1 | 1 Length | 1 Engine | 1 Quantity | 1 Propellant ID | 1 Propellant Ox | 1 Propellant Fuel | 1 Burn Rate | 1 Flow Rate | 1 Empty | 1 Propellant | 1 Gross | 1 Upper | 1 Net | 1 VAC Thrust | 1 VAC Specific Impulse | 1 VAC T-W Ratio | 1 SL Thrust | 1 SL Specific Impulse | 1 SL T-W Ratio | Stage 2 | 2 Length | 2 Engine | 2 Quantity | 2 Propellant ID | 2 Propellant Ox | 2 Propellant Fuel | 2 Burn Rate | 2 Flow Rate | 2 Empty | 2 Propellant | 2 Gross | 2 Upper | 2 Net | 2 VAC Thrust | 2 VAC Specific Impulse | 2 VAC T-W Ratio | 2 SL Thrust | 2 SL Specific Impulse | 2 SL T-W Ratio | Stage 3 | 3 Length | 3 Engine | 3 Quantity | 3 Propellant ID | 3 Propellant Ox | 3 Propellant Fuel | 3 Burn Rate | 3 Flow Rate | 3 Empty | 3 Propellant | 3 Gross | 3 Upper | 3 Net | 3 VAC Thrust | 3 VAC Specific Impulse | 3 VAC T-W Ratio | 3 SL Thrust | 3 SL Specific Impulse | 3 SL T-W Ratio | Stage 4 | 4 Length | 4 Engine | 4 Quantity | 4 Propellant ID | 4 Propellant Ox | 4 Propellant Fuel | 4 Burn Rate | 4 Flow Rate | 4 Empty | 4 Propellant | 4 Gross | 4 Upper | 4 Net | 4 VAC Thrust | 4 VAC Specific Impulse | 4 VAC T-W Ratio | 4 SL Thrust | 4 SL Specific Impulse | 4 SL T-W Ratio | Stage 5 | 5 Length | 5 Engine | 5 Quantity | 5 Propellant ID | 5 Propellant Ox | 5 Propellant Fuel | 5 Burn Rate | 5 Flow Rate | 5 Empty | 5 Propellant | 5 Gross | 5 VAC Thrust | 5 VAC Specific Impulse | 5 VAC T-W Ratio | 5 SL Thrust | 5 SL Specific Impulse | 5 SL T-W Ratio |