| China, CALT | Naga-L | |||
|
Overall Vehicle |
Operational | from | 2017 | |
| to | ||||
| Orbital flights | ||||
| Payload weight | t | SSO | 0.50 | |
| Gross liftoff weight | t | 98.227 | ||
| Gross propellant weight | t | 87.96 | ||
| Total length | m | 29.219 | ||
| Max. diameter (span) | m | |||
| Total liftoff thrust (s.l.) | kN | 1,199.6 | ||
| Total impulse (vac) | MN*s | 300.1 | ||
|
Fairing |
Total length | m | 5.279 | |
| Diameter | m | 3.00 | ||
| Total weight | t | 0.88 | ||
|
Stage 2 |
Name | L-10 | ||
| Length | m | ~7.10 | ||
| Diameter | m | 3.00 | ||
| Liftoff weight | t | 13.183 | ||
| Propellant weight | t | 10.498 | ||
| Engines | YF-75D | |||
| Propellant | LH2/LOX | |||
| Total thrust (vac) | kN | 83.27 | ||
| Specific impulse (vac) | N*s/kg | 4340 | ||
| Burn time | s | 547 | ||
| Total impulse (vac) | MN*s | 45.6 | ||
| Stage 1 |
Name |
L-77 (K3-0) | ||
| Length (with adapter) | m | ~16.8 | ||
| Diameter | m | 3.35 | ||
| Liftoff weight | t | 83.664 | ||
| Propellant weight | t | 77.460 | ||
| Engines | YF-100 | |||
| Propellant | Kerosene/LOX | |||
| Total thrust ( s.l.) | kN | 1,199.6 | ||
| Specific impulse ( s.l.) | N*s/kg | 2942 | ||
| Burn time | s | 190 | ||
| Total impulse (vac) | MN*s | 254.5 | ||