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Space Technology 5 (ST5) of the NASA New Millennium program was a test of ten new technologies aboard a group of microsatellites. Developed by NASA Goddard Space Flight Center, the three individual small spacecraft were launched together from the belly of a Lockheed L-1011 aboard the Pegasus XL rocket, on 22 March 2006. One technology involved antennas…
Technology, Mission objectives & Overview
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space technology nasa st5 mission flight 2006 center system pegasus 22 aboard developed new xl rocket 2002 retrieved technologies march
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Space Technology 5 | Apogee altitude | 4,500 km (2,800 mi) | 1.00 | infobox |
| Space Technology 5 | Band | X-Band | 1.00 | infobox |
| Space Technology 5 | Bandwidth | 1 Kbps / 1 or 100 Kbps | 1.00 | infobox |
| Space Technology 5 | COSPAR ID | 2006-008A through 2006-008C | 1.00 | infobox |
| Space Technology 5 | Deactivated | June 30, 2006 (2006-06-30) | 1.00 | infobox |
| Space Technology 5 | Eccentricity | 0.239 | 1.00 | infobox |
| Space Technology 5 | Inclination | 105.6° | 1.00 | infobox |
| Space Technology 5 | Launch mass | 25 kilograms (55 lb) | 1.00 | infobox |
| Space Technology 5 | Manufacturer | UCLA Kennedy Space Center New Mexico State University Physical Science Laboratory | 1.00 | infobox |
| Space Technology 5 | Mission duration | 20 years, 5 months and 2 days (in orbit) | 1.00 | infobox |
| Space Technology 5 | Operator | NASA / GSFC | 1.00 | infobox |
| Space Technology 5 | Perigee altitude | 300 km (190 mi) | 1.00 | infobox |
| Space Technology 5 | Power | ≈20–25 W @ 9–10 V | 1.00 | infobox |
| Space Technology 5 | Reference system | Geocentric | 1.00 | infobox |
| Space Technology 5 | Regime | Sun synchronous | 1.00 | infobox |
| Space Technology 5 | Rocket | Pegasus XL | 1.00 | infobox |
| Space Technology 5 | SATCAT no. | 28980 through 28982 | 1.00 | infobox |
| Space Technology 5 | Website | nmp.jpl.nasa.gov/st5 | 1.00 | infobox |
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