| Name | Manufacturer | Operator | Stages | Crew | Payload Mass | Status | Image |
| Altair | Northrop Grumman | NASA | Descent, Ascent | 4 | 14,500 kg | | |
| Apollo Lunar Module | Grumman | NASA | Descent, Ascent | 2 | | | |
| Boeing Lunar Lander | Boeing | Boeing, NASA | Descent, Ascent | | | | |
| Dynetics HLS | Dynetics | Dynetics, NASA | Single-stage with drop tanks | 2-4 | | | |
| Blue Moon Mark 2 | Blue Origin, Lockheed Martin, Northrop Grumman, Draper Laboratory | Blue Origin, Lockheed Martin, Northrop Grumman, Draper Laboratory, NASA | Transfer, Lander/Ascent | 4 | | | |
| Lanyue Lunar Lander | CAST | CMSA | Descent propulsion stage, Lander/Ascent | 2 | | | |
| LK | RSC Energia/Yuzhnoye Design Office | Soviet Union | Descent, Ascent | 1 | | | |
| Lockheed Martin Lunar Lander | Lockheed Martin | Lockheed Martin, NASA | Single-stage | 4 | 1,000 kg |
| |
| Starship | SpaceX | SpaceX | Single-stage | | | | |
| Starship HLS | SpaceX | NASA, SpaceX | Single-stage | 4 | 100–200 t | | |
| BIS Lunar Lander | | British Interplanetary Society | Single-stage | 3 | | Studies | |
| Von Braun Lunar Lander | | US | Single-stage with drop tanks | 20 | 259 metric tons | Study | |
| Horizon LERV | | US Army | Descent, Ascent | 10 - 16 | 2,700 - 22,000 kg | Study | |
| Lunex Lunar Lander | | US Air Force | Descent, Ascent | 3 | 20,500 kg | Study | |
| Gemini lunar lander | | NASA Langley Research Center, | Single | 1 | | | |
| LEK | | Soviet Union, | Descent, Ascent, Reentry | 3 | | | |
| FLO Eagle lander | | NASA | Descent, Ascent | 4 | 5,000 kg | | |