Generated by DeepSeek V3.2| Clementine (spacecraft) | |
|---|---|
| Name | Clementine |
| Mission type | Lunar orbiter / Asteroid flyby technology demonstration |
| Operator | NASA / Ballistic Missile Defense Organization |
| COSPAR ID | 1994-004A |
| SATCAT | 22973 |
| Mission duration | 115 days |
| Spacecraft | Clementine |
| Manufacturer | Naval Research Laboratory |
| Launch mass | 424 kg |
| Power | 360 watts |
| Launch date | 25 January 1994, 16:34 UTC |
| Launch rocket | Titan II (23)G |
| Launch site | Vandenberg SLC-4W |
| Last contact | May 1994 |
| Orbit reference | Selenocentric orbit |
| Orbit regime | Polar |
| Orbit periapsis | 425 km |
| Orbit apoapsis | 2,950 km |
| Orbit inclination | 90° |
| Orbit period | 300 minutes |
| Apsis | selene |
Clementine (spacecraft). Clementine was a joint project between the Ballistic Missile Defense Organization (BMDO) and NASA, designed as a technology demonstration for advanced lightweight sensors and spacecraft components. Launched in 1994, its primary mission was to map the Moon in multiple wavelengths and conduct a flyby of the near-Earth asteroid 1620 Geographos. Although the asteroid rendezvous failed, the spacecraft returned a wealth of groundbreaking data about the lunar surface, providing the first global multispectral maps and suggesting evidence of water ice in permanently shadowed craters.
The mission was conceived as a low-cost, high-risk demonstration for the Strategic Defense Initiative and was managed by the Naval Research Laboratory. Its objectives were to test new lightweight imaging sensors, including a LIDAR system, and to validate advanced spacecraft components during a long-duration deep space flight. The trajectory involved a two-month mapping orbit around the Moon before a planned departure and flyby of 1620 Geographos. This ambitious plan aimed to gather scientific data for NASA while proving technologies with potential applications for the Ballistic Missile Defense Organization.
The spacecraft bus was built by the Naval Research Laboratory and had an octagonal structure, with a mass of just 424 kilograms. It was powered by a single solar panel and a nickel-hydrogen battery. The sensor suite was its most notable feature, including two star tracker cameras, a high-resolution LIDAR altimeter, and a sophisticated set of cameras covering wavelengths from ultraviolet to near-infrared. This array, particularly the UV/Vis camera and the NIR camera, was designed for detailed mineralogical mapping of the lunar surface.
After entering a polar orbit around the Moon in February 1994, Clementine systematically mapped the entire surface over 71 days. Its multispectral imaging provided the first global digital maps of the Moon's topography and composition, revealing the complex geology of features like the South Pole–Aitken basin. The most provocative discovery came from its bistatic radar experiment, where radio signals were bounced off shadowed regions near the lunar south pole; the return signatures were consistent with the presence of water ice in permanently dark craters, a hypothesis later supported by missions like Lunar Prospector.
Following its lunar mission, a spacecraft malfunction on May 7, 1994, caused a thruster to fire until it expended all its fuel, sending the probe into an uncontrolled spin. This failure prevented the planned trajectory correction burn needed to reach 1620 Geographos. The malfunction, attributed to a software error, ended the asteroid flyby phase of the mission. Despite this, the spacecraft had already completed its primary lunar objectives, and the Ballistic Missile Defense Organization declared the technology demonstration a success.
Clementine is widely regarded as a pathfinder for the "Faster, Better, Cheaper" era of NASA planetary exploration. Its data fundamentally altered lunar science, providing a foundational dataset for subsequent missions like Lunar Reconnaissance Orbiter. The potential detection of water ice revolutionized plans for future lunar exploration and sustained human presence. The mission proved the viability of lightweight, capable spacecraft for deep space, directly influencing the design of later probes such as those in the Discovery Program.
Category:NASA space probes Category:1994 in spaceflight Category:Lunar orbiters