 Replica of aLunar Orbiter spacecraft | |||||||||||
| Mission type | Lunar orbiter | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Operator | NASA | ||||||||||
| COSPAR ID | 1966-100A | ||||||||||
| SATCATno. | 2534 | ||||||||||
| Website | science.nasa.gov | ||||||||||
| Mission duration | 11 months, 5 days | ||||||||||
| Spacecraft properties | |||||||||||
| Manufacturer | Langley Research Center | ||||||||||
| Launch mass | 385.6 kg (850 lb)[1] | ||||||||||
| Dimensions | 3.72 × 1.65 × 1.5 m (12.2 × 5.4 × 4.9 ft)[2] | ||||||||||
| Power | 375 watts[2] | ||||||||||
| Start of mission | |||||||||||
| Launch date | November 6, 1966, 23:21:00 (1966-11-06UTC23:21Z) UTC | ||||||||||
| Rocket | Atlas SLV-3 Agena-D | ||||||||||
| Launch site | Cape CanaveralLC-13 | ||||||||||
| End of mission | |||||||||||
| Disposal | Deorbited | ||||||||||
| Decay date | October 11, 1967, 07:12:54 (1967-10-11UTC07:12:55) UTC | ||||||||||
| Orbital parameters | |||||||||||
| Reference system | Selenocentric | ||||||||||
| Semi-major axis | 2,694 km (1,674 mi) | ||||||||||
| Eccentricity | 0.35 | ||||||||||
| Periselene altitude | 1,790 km (1,110 mi) | ||||||||||
| Aposelene altitude | 3,598 km (2,236 mi) | ||||||||||
| Inclination | 11.9 degrees | ||||||||||
| Period | 208.07 minutes | ||||||||||
| Epoch | November 9, 1966, 19:00:00 UTC[2] | ||||||||||
| Lunar orbiter | |||||||||||
| Orbital insertion | November 10, 1966 | ||||||||||
| Impact site | 3°00′N119°06′E / 3.0°N 119.1°E /3.0; 119.1 | ||||||||||
| Orbits | 2,346 | ||||||||||
| Transponders | |||||||||||
| Frequency | 2295MHz[2] | ||||||||||
| |||||||||||
The 1966Lunar Orbiter 2robotic spacecraft mission, part of theLunar Orbiter Program,[8] was designed primarily to photograph smooth areas of thelunar surface for selection and verification of safe landing sites for theSurveyor andApollo missions. It was also equipped to collectselenodetic, radiation intensity, andmicrometeoroid impact data.
The spacecraft was placed in acislunar trajectory and injected into an elliptical near-equatorial lunar orbit for data acquisition after 92.6 hours' flight time. The initial orbit was 196 by 1,850 kilometres (122 mi × 1,150 mi) at an inclination of 11.8 degrees. The perilune was lowered to 49.7 kilometres (30.9 mi) five days later after 33 orbits. A failure of the amplifier on the final day of readout, December 7, resulted in the loss of six photographs. On December 8, 1966 the inclination was altered to 17.5 degrees to provide new data on lunar gravity.
The spacecraft acquired photographic data from November 18 to 25, 1966, and readout occurred through December 7, 1966. A total of 609 high-resolution and 208 medium-resolution frames were returned, most of excellent quality with resolutions down to 1 metre (3 ft 3 in).[9][10] These included a spectacular oblique picture ofCopernicus crater, which was dubbed by the news media as one of the great pictures of the century. The photo was taken on the 23rd November at an altitude of 45km.[11] Accurate data were acquired from all other experiments throughout the mission. Three micrometeorite impacts were recorded. The spacecraft was used for tracking purposes until it impacted upon the lunar surface on command at 3.0 degrees N latitude, 119.1 degrees E longitude (selenographic coordinates) on October 11, 1967.
In 2011, NASA'sLunar Reconnaissance Orbiter Camera (LROC) was able to locate and image the precise impact point of the spacecraft. The debris from an impact angle of 45 degrees or more spreads out like butterfly wings.[12]
| Lunar Photographic Studies | Evaluation of Apollo and Surveyor landing sites |
|---|---|
| Meteoroid Detectors | Detection of micrometeoroids in the lunar environment |
| Caesium Iodide Dosimeters | Radiation environment en route to and near the Moon |
| Selenodesy | Gravitational field and physical properties of the Moon |
| Missions |  | |
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| Related | ||
