| class="wikitable sortable" |
| Name | Manufacturer | Operator (program and operational timeline) | Stages | Crew | Payload Mass | Status | Image |
|---|
| Altair | Northrop Grumman | NASA (Constellation, 2005–2009) | Descent, Ascent | 4 | 14,500 kg (32,000 lb) | {{No|Canceled}} | 120px |
| Apollo Lunar Module | Grumman | NASA (Apollo, 1969–1972) | Descent, Ascent | 2 | | {{Included|Retired}} | 120px |
| Boeing Lunar Lander | Boeing | Boeing, NASA (Artemis, 2017–present) | Descent, Ascent | | | {{No|Rejected}} | [https://boeing.mediaroom.com/2019-11-05-Boeing-Proposes-Fewest-Steps-to-the-Moon-for-NASAs-Human-Lander] |
| Dynetics HLS | Dynetics | Dynetics, NASA (Artemis, 2017–present) | Single-stage with drop tanks | 2-4 | | {{No|Rejected}} | [https://www.dynetics.com/_images/banners/dyn-banner-119965424e.jpg] |
| 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 | | {{Planned}} | [https://encrypted-tbn0.gstatic.com/images?q=tbn:ANd9GcRU2Q5zx2RhgcpC6Lqona-iowR_8gEke53B6Rbz6roOFaOBGe6Cz-VAkREp&s=10] |
| Lanyue Lunar Lander | CAST | CMSA (CLEP) | Descent propulsion stage, Lander/Ascent | 2 | | {{Planned}} | 120px |
| LK | RSC Energia/Yuzhnoye Design Office | Soviet Union (N1-L3, 1969-1974) | Descent, Ascent | 1 | | {{No|Canceled}} | 120px |
| Lockheed Martin Lunar Lander | Lockheed Martin | Lockheed Martin, NASA (Artemis, 2017–present) | Single-stage | 4 | 1,000 kg (2,200 lb) | {{No|Rejected}}
(elements incorporated into Blue Moon Mk 2) | [https://www.flickr.com/photos/lockheedmartin/44167182465/in/album-72157671935059557/] |
| Starship | SpaceX | SpaceX | Single-stage | | | {{Planned}} | 120px [https://www.nasa.gov/sites/default/files/thumbnails/image/spacex_1.jpg] |
| Starship HLS | SpaceX | NASA (Artemis, 2017–present), SpaceX | Single-stage | 4 | 100–200 t (220,000–440,000 lb) | {{Planned}} | [https://www.nasa.gov/sites/default/files/thumbnails/image/for_press_release.jpg] |
BIS Lunar Lander[{{Cite web|url=http://www.astronautix.com/b/bislunarlander.html|archive-url=https://web.archive.org/web/20160820165259/http://www.astronautix.com/b/bislunarlander.html|url-status=dead|archive-date=August 20, 2016|title=BIS Lunar Lander|website=www.astronautix.com}}] | | British Interplanetary Society | Single-stage | 3 | | Studies (1939, 1947) | |
Von Braun Lunar Lander[{{Cite web|url=http://www.astronautix.com/v/vonbraunlunarlander.html|archive-url=https://web.archive.org/web/20160820150934/http://www.astronautix.com/v/vonbraunlunarlander.html|url-status=dead|archive-date=August 20, 2016|title=Von Braun Lunar Lander|website=www.astronautix.com}}] | | US (1977) | Single-stage with drop tanks | 20 | 259 metric tons (with a crew of 10) | Study (1952) | |
Horizon LERV[{{Cite web|url=http://www.astronautix.com/h/horizonlerv.html|archive-url=https://web.archive.org/web/20161228020518/http://astronautix.com/h/horizonlerv.html|url-status=dead|archive-date=December 28, 2016|title=Horizon LERV|website=www.astronautix.com}}] | | US Army (Project Horizon, 1966) | Descent, Ascent | 10 - 16 | 2,700 - 22,000 kg | Study (1959) | 120px |
Lunex Lunar Lander[{{Cite web|url=http://www.astronautix.com/l/lunexlunarlander.html|archive-url=https://web.archive.org/web/20161228024113/http://astronautix.com/l/lunexlunarlander.html|url-status=dead|archive-date=December 28, 2016|title=Lunex Lunar Lander|website=www.astronautix.com}}] | | US Air Force (Lunex Project, 1967) | Descent, Ascent | 3 | 20,500 kg | Study (1958–1961) | 120px |
| Gemini lunar lander | | NASA Langley Research Center, (Project Gemini, 1963) | Single | 1 | | {{No|Canceled}} | 120px |
LEK[{{cite web |url=http://www.astronautix.com/craft/lek.htm |title=LEK |website=www.astronautix.com |access-date=12 January 2022 |archive-url=https://web.archive.org/web/20060316185549/http://www.astronautix.com/craft/lek.htm |archive-date=16 March 2006 |url-status=dead}}] | | Soviet Union, (Zvezda Moon base, 1974) | Descent, Ascent, Reentry | 3 | | {{No|Canceled}} | |
| FLO Eagle lander | | NASA (Space Exploration Initiative, 1992–93) | Descent, Ascent | 4 | 5,000 kg | {{No|Canceled}} | 120px |
