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SNAP-10A (Systems for Nuclear Auxiliary Power, aka Snapshot for Space Nuclear Auxiliary Power Shot, also known as OPS 4682) was a US experimental nuclear powered satellite launched into space in 1965 as part of the SNAPSHOT program. The test marked both the world's first operation of a nuclear reactor in orbit, and the first operation of an ion thruster…
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nuclear reactor power snap system systems space international orbit also atomics auxiliary snapshot first fission energy program ion launch used
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| SNAP-10A | Apogee altitude | 1,317 km (818 mi) | 1.00 | infobox |
| SNAP-10A | COSPAR ID | 1965-027A | 1.00 | infobox |
| SNAP-10A | Decay date | c. 2965 | 1.00 | infobox |
| SNAP-10A | Eccentricity | 0.00319 | 1.00 | infobox |
| SNAP-10A | Epoch | 3 April 1965 | 1.00 | infobox |
| SNAP-10A | Inclination | 90.2° | 1.00 | infobox |
| SNAP-10A | Last contact | 16 May 1965 | 1.00 | infobox |
| SNAP-10A | Launch date | 3 April 1965, 21:25 (1965-04-03UTC21:25) | 1.00 | infobox |
| SNAP-10A | Launch mass | 440 kg (970 lb) | 1.00 | infobox |
| SNAP-10A | Launch site | Vandenberg AFB, PALC2-4 | 1.00 | infobox |
| SNAP-10A | Manufacturer | Atomics International | 1.00 | infobox |
| SNAP-10A | Mission duration | 43 days (achieved) 61 years, 4 months, 19 days (in orbit) | 1.00 | infobox |
| SNAP-10A | Mission type | Engineering | 1.00 | infobox |
| SNAP-10A | Operator | USAF | 1.00 | infobox |
| SNAP-10A | Perigee altitude | 1,268 km (788 mi) | 1.00 | infobox |
| SNAP-10A | Period | 111.4 minutes | 1.00 | infobox |
| SNAP-10A | Reference system | Geocentric | 1.00 | infobox |
| SNAP-10A | Regime | Low Earth | 1.00 | infobox |
| SNAP-10A | Rocket | Atlas-Agena D | 1.00 | infobox |
| SNAP-10A | SATCAT no. | 01314 | 1.00 | infobox |
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