2006-008A
Each Nanosat Constellation Trailblazer is 25 kg, 0.52m dia 0.48 high oct prism with an extendable boom for 1.0m? span. Three satellites on a single launch to 300 x 4500 km x 97 deg on Pegasus XL from Vandenberg. Built by GSFC. Will study magnetosphere; spacecraft highly magnetically clean to allow short mag booms.
| ST5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2006 Mar 14 | 1327 | L1011 T/O V RW30/12 | |
| 1428 | Abort | ||
| 1448s | Land on RW12 | ||
| 2006 Mar 22 | 1304 | L1011 T/O V RW30/12 | |
| 1403:45 | Drop | ||
| 1403:50 | T+0:05 Stage 1 on 70s | ||
| 1405:02 | T+1:17 Stage 1 burnout | ||
| Stage 1 sep | |||
| 1405:16 | T+1:31 Stage 2 on | ||
| 1405:55 | T+2:10 Fairing sep, 115 km | ||
| 1406:29 | T+2:44 St 2 burnout, 156 km | ||
| 1409:02 | T+5:17 Stage 2 sep | ||
| 1409:02 | T+5:17 Stage 3 burn 283 km | ||
| 1410:09? | T+6:24? Stage 3 burnout | ||
| 1413:16s | T+9:31 ST5-FWD sep S+0 | ||
| 1416:26 | T+12:41 ST5-2 sep S+200s | ||
| 1419:36 | T+15:51 ST5-3 sep S+390s | 301 x 4568 x 105.6 | |
| Pegasus CCAM | |||
| 1532 | 298 x 4554 x 105.6 | ||
| 2008 Jun 30 | end of ops | ||
Payload:
- X-band transponder, Aero Astro comms system
- CULPRIT Low power microelectronic device, CMOS ultra low power radiation tolerant logic.
- Cold gas microthruster, Fine attitude adjustment
- Lithium ion power system
- Magnetometer booms, 0.36m long
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