1994-028A
MSTI 2 was built by Spectrum Astro for USAF Phillips Lab using the SA200S series bus. This added a hydrazine propulsion system to the MSTI-1 vehicle. The 168 kg octagonal box-shaped, 3-axis stabilized satellite was designed for theater ballistic missile acquisition and tracking, and was originally intended to watch tests of the LEAP projectile. It observed a Minuteman launch from Vandenberg in Jun 1994.
| MSTI 2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1994 May 9 | 0247 | Launch by Scout G-1 | V SLC5 |
| T+1:24 Stage 1 burnout | |||
| T+1:28 St 1 sep | |||
| T+1:28 St 2 burn | |||
| T+2:09 St 2 burnout | |||
| T+2:20 Fairing sep | |||
| T+2:22 St 2 sep, St 3 burn | |||
| T+3:10 St 3 burnout | |||
| T+10? St 3 sep | |||
| 0257? | T+10? St 4 burn | ||
| 0257? | T+10? Stage 4 burnout | ||
| 0304 | T+17 min Star 20 sep, in orbit | ||
| 360 x 461 x 96.8 | |||
| 1994 Jun 8 | 1630 | Observed VAFB Minuteman launch | |
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