| Institudo Nacional de Tecnica Aerospacial |
Capricornio |
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|
Overall Vehicle |
Operational | from | ||
| to | ||||
| Orbital flights | canceled | |||
| Payload weight | t | LEO | 0.10 | |
| Gross liftoff weight | t | 15.035 | ||
| Gross propellant weight | t | 12.700 | ||
| Total length | m | 18.25 | ||
| Max. diameter (span) | m | |||
| Total liftoff thrust (s.l.) | kN | 385.2 | ||
| Total impulse (vac) | MN*s | 33.8 | ||
|
Fairing |
Total length | m | ||
| Diameter | m | 0.83 | ||
| Total weight | t | |||
| Stage 3 | Name | Mizar-B | ||
| Length | m | 2.10 | ||
| Diameter | m | 0.83 | ||
| Liftoff weight | t | 0.717 | ||
| Propellant weight | t | 0.607 | ||
| Engines | I-100 | |||
| Propellant | HTPB | |||
| Total thrust (vac) | kN | 50.29 | ||
| Specific impulse (vac) | N*s/kg | 2785 | ||
| Burn time | s | 33.8 | ||
| Total impulse (vac) | MN*s | 1.7 | ||
| Stage 2 |
Name |
DENEB-F TVC | ||
| Length | m | 3.00 | ||
| Diameter | m | 0.83 | ||
| Liftoff weight | t | 2.549 | ||
| Propellant weight | t | 2.124 | ||
| Engines | I-300 | |||
| Propellant | HTPB | |||
| Total thrust (vac) | kN | 167.9 | ||
| Specific impulse (vac) | N*s/kg | 2814 | ||
| Burn time | s | 35.6 | ||
| Total impulse (vac) | MN*s | 6.0 | ||
|
Stage 1 |
Name | Castor IVB | ||
| Length (+adapter) | m | 8.99 | ||
| Diameter | m | 1.02 | ||
| Liftoff weight | t | 11.470 | ||
| Propellant weight | t | 9.969 | ||
| Engines | TX- 859 TVC | |||
| Propellant | solid TP-H8299 | |||
| Total thrust (s.l.) | kN | 385.2 | ||
| Specific impulse (s.l.) | N*s/kg | 2337 | ||
| Burn time | s | 60.5 | ||
| Total impulse (vac) | MN*s | 26.1 | ||