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McCandless Lunar Lander
| Manufacturer | Lockheed Martin |
|---|---|
| Designer | Lockheed Martin |
| Country of origin | United States |
| Operator | Lockheed Martin |
| Applications | Commercial cargo lander |
| Specifications | |
| Spacecraft type | Robotic lunar lander |
| Payload capacity | 250 kg (550 lb) [1] |
| Power | 400 W [1] from a single solar array on a boom |
| Design life | 1 lunar day (14 Earth days) [1] |
| Dimensions | |
| Length | Height: >2 m (6 ft 7 in) [1] |
| Diameter | 3 m (9.8 ft) [1] |
| Production | |
| Status | Designed |
| On order | 0 |
| Built | 0 |
| Related spacecraft | |
| Derived from | Phoenix and InSight landers |
McCandless Lunar Lander, also known as the McCandless Lunar Delivery Service, is a concept for a robotic lunar lander proposed as one of the commercial cargo vehicles for NASA's Commercial Lunar Payload Services (CLPS). The lander was proposed to NASA for funding by the aerospace company Lockheed Martin, and it is based on the successful Mars landers Phoenix and InSight.
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