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Sighter Launch Vehicle
The Sighter vehicle consists of a solid fuel motor 83mm in diameter and 1.4m in length to which ASRI has designed and attached various fins and nosecone modules. With a payload of 3kg, the Sighter has an apogee of 5.9km in about 40 seconds, experiencing a vicious 55g and 491m/s (Mach 1.4) during the flight.
Launch Log
| Date | RecordID | LaunchVehicle | LaunchArea | Apogee | Stabilized | Purpose |
|---|---|---|---|---|---|---|
| 1995:05:21:0140 | S2-WO1-19950521-1110 | Sighter | Fin | |||
| 1995:05:21:???? | S1-WO1-19950521-D | Sighter | Fin | |||
| 1995:05:22:0030 | S3-WO1-19950522-1000 | Sighter | Fin | |||
| 1995:05:25:0030 | S4-WO1-19950525-1000 | Sighter | Fin | |||
| 1995:08:??:???? | S5-WB1-19950800-0000 | Sighter | Fin | |||
| 1995:08:??:???? | S6-WB1-19950800-0000 | Sighter | Fin | |||
| 1995:08:??:???? | S7-WB1-19950800-0000 | Sighter | Widebay | Fin | ||
| 1995:08:??:???? | S8-WB1-19950800-0000 | Sighter | Widebay | Fin | ||
| 1997:10:05:1400 | S1 | sighter | LA-9 | Unknown | None | MOTOR SHORT NON SEPARATING PAYLOAD |
| 1997:10:05:1430 | S2 | sighter | LA-9 | MOTOR LONG NON SEPARATING PAYLOAD |
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