You are hereLaunch Vehicle - Corella
Launch Vehicle - Corella
General Information
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Corella was a sounding rocket used to study the upper atmosphere. Two (2) launches were made. |
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| Purpose: | Atmospheric Research |
| Period of Use: | 1975 - 1976 |
| Payload Mass: | 100 lb |
| Apogee: | 610000 ft |
Motor Details
| Ignition | Motor | Impulse | Burn Time | |
| Stage 1 | T+0 | INDUS | 96000 lb.sec | 4.5 s |
| Stage 2 | T+14 | DORADO | 38500 lb.sec | 4.3 s |
