| Manufacturer |
ArianeGroup |
| Function |
A62: Medium-lift launch vehicle
A64: Heavy-lift launch vehicle |
| Stages |
2 |
| Length |
63 m |
| Diameter |
5.4 m |
| Mass |
A62: 530,000 kg A64: 860,000 kg |
| Capacity: |
Payload to LEO |
| Mass |
A62: 10,350 kg A64: 21,650 kg |
| Capacity: |
Payload to GTO |
| Orbital inclination |
6° |
| Mass |
A62: 4,500 kg A64: 11,500 kg |
| Capacity: |
Payload to GEO |
| Orbital inclination |
0° |
| Mass |
A64: 5,000 kg |
|
| Stage |
1st Stage |
2nd Stage |
Boosters 2 or 4 |
| Length (m) |
- |
- |
- m |
| Diameter (m) |
5.4 m |
5.4 m |
3 m |
| Propeellant Mass (kg) |
140,000 kg |
31,000 kg |
142,000 kg |
| Engine |
1x Vulcain 2.1 |
1x Vinci |
- |
| Max Thrust |
1,370 kN |
1,370 kN |
A62: 7,000 kN A64: 14,000 kN |
| Burn time |
468 sec |
up to 900 sec |
130 sec |
| Propellants |
LOX/LH2 |
LOX/LH2 |
HTPB/AP/Al |
|