List of crewed Mars mission plans
This list of crewed Mars mission plans is a listing of concept studies for a crewed mission to Mars during the 20th and 21st centuries. It is limited to studies done with engineering and scientific knowledge about the capabilities of then current technology, typically for high-budget space agencies like NASA. Mission profiles include crewed flybys, crewed landers, or other types of Mars system encounter strategies.
Concepts
Many mission concepts for expeditions to Mars were proposed in the late 20th century. David Portree's history volume Humans to Mars: Fifty Years of Mission Planning, 1950–2000 discusses many of these. Portree notes that every 26 Earth months a lower energy Earth to Mars transfer opportunity opens, so missions typically coincide with one of these windows. In addition, the lowest available transfer energy varies on a roughly 16-year cycle, with a minimum in the 1969 and 1971 launch windows, rising to a peak in the late 70s, and hitting another low in 1986 and 1988. Also of note, the Mariner 4 Mars flyby in 1965 provided radically more accurate data about the planet; a surface atmospheric pressure of about 1% of Earth's and daytime temperatures of −100 degrees Celsius were estimated. No magnetic field or Martian radiation belts were detected. The new data meant redesigns for planned Martian landers, and showed life would have a more difficult time surviving there than previously anticipated. Later NASA probes in the 1970s, 80s, and 90s confirmed the findings about Mars environmental conditions.The first engineering analysis of a crewed mission to Mars was made by Wernher von Braun in 1948. It was originally published as Das Marsprojekt in West Germany in 1952, and as The Mars Project in English in the United States in 1953. Von Braun's Mars "flotilla" included ten 4,000-ton ships with 70 crew members. The expected launch year was 1965.
List
The list is in semi-chronological order, with some groupings, as variation can exist in the dating of a given plan. Various references were consulted. LEO mass refers to how much hardware must be put in low Earth orbit for the mission. For comparison, the low Earth orbit payload capacity per launch of the U.S. Space Shuttle is about 25 metric tons, and that of the Saturn V, 120 metric tons.Name | Crew | LEO mass | Year announced | Suggested launch year | Sources |
Von Braun Mars 1952 | 70 | 37,200 | 1952 | 1965 | |
Stuhlinger Mars 1954–1957 | 20 | 660 | 1954 | 1980 | |
Von Braun Mars 1956 | 12 | 3,400 | 1956 | 1970 | |
Martian Piloted Complex 1958–1962 | 6 | 1,630 | 1958 | 1975 | |
TMK-1 1959 | 3 | 75 | 1959 | 1971 | |
Bono Mars 1960 | 8 | 800 | 1960 | 1971 | |
NASA Lewis Mars 1960 | 6 | 614 | 1960 | 1971 | |
TMK-2 | 2 | 75 | 1960 | 1971 | |
EMPIRE Aeronutronic 1962 | 6 | 227 | 1962 | 1970 | |
Stuhlinger Mars 1962 | 15 | 1,800 | 1962 | 1975 | |
EMPIRE General Dynamics 1962 | 8 | 900 | 1962 | 1975 | |
EMPIRE Lockheed 1962 | 3 | 100 | 1962 | 1974 | |
Faget Mars 1963 | 6 | 1,140 | 1963 | ||
Faget Mars 1963 | 6 | 270 | 1963 | ||
TRW Mars Expedition 1963 | 6 | 650 | 1963 | 1975 | |
UMPIRE Douglas 1964 | 6 | 450 | 1964 | 1975 | |
Project Deimos | 6 | 3,965 | 1964 | 1986 | |
Douglas MORL Mars Flyby 1965 | 3 | 360 | 1965 | 1973 | |
NASA JAG Manned Mars Flyby 1966 | 4 | 1966 | 1975 | ||
NASA NERVA-Electric Mars 1966 | 5 | 1,552 | 1966 | 1986 | |
Korolev KK 1966 | 3 | 150 | 1966 | 1980 | |
Titus FLEM 1966 | 3 | 118 | 1966 | 1985 | |
Stuhlinger Mars 1966 | 2,788 | 1966 | |||
Boeing IMIS 1968 | 6 | 1,226 | 1968 | 1985 | |
Mars Expeditionary Complex 1969 | 3 | 150 | 1969 | 1980 | |
Von Braun Mars 1969 | 12 | 1,455 | 1969 | 1981 | |
NASA Mars Expedition 1971 | 6 | 1,900 | 1971 | 1987 | |
Mars in 30 Days | 5 | 2,041 | 1972 | ||
MK-700 1972 | 2 | 1,400 | 1972 | 1980 | |
Chelomei 1975 | 2 | 250 | 1975 | 1980 | |
British Interplanetary Society Mars 1982 | 8 | 1,300 | 1982 | ||
Planetary Society Mars Expedition 1983 | 4 | 160 | 1983 | 2003 | |
Case for Mars II 1984 | 30 | 1,900 | 1984 | 2007 | |
NASA-LANL Manned Mars Flyby 1985 | 350 | 1985 | |||
Paine 1986 | 1986 | 2026 | |||
NPO Energia Mars 1986 | 4 | 365 | 1986 | 2000 | |
NASA Ride Report 1987 | 6 | 210 | 1987 | 2004 | |
NASA Mars Evolution 1988 | 8 | 330 | 1988 | 2013 | |
NASA Mars Expedition 1988 | 8 | 1,628 | 1988 | 2007 | |
NASA Phobos Expedition 1988 | 4 | 765 | 1988 | 2003 | |
NASA 90 Day Study 1989 | 4 | 980 – 1,300 | 1989 | 2017 | |
NPO Energia Mars 1989 | 4 | 355 | 1989 | 2001 | |
Mars Evolution 1989 | 5 | 1989 | 2007 | ||
NASA Mars Expedition 1989 | 3 | 780 | 1989 | 2004 | |
Mars Direct | 4 | 220 | 1991 | 1997 | |
STCAEM CAB 1991 | 4 | 800 | 1991 | 2016 | |
STCAEM NEP 1991 | 4 | 500 | 1991 | 2016 | |
STCAEM NTR 1991 | 4 | 800 | 1991 | 2016 | |
STCAEM SEP 1991 | 4 | 410 | 1991 | 2016 | |
NASA Synthesis Study 1991 | 6 | 1,080 | 1991 | 2014 | |
International Space University 1991 | 8 | 1991 | 2016 | ||
NASA Design Reference Mission 1.0 1993 | 6 | 900 | 1993 | 2007 | |
Kurchatov Mars 1994 | 5 | 800 | 1994 | 2010 | |
Zubrin Athena | 2 | 100 | 1996 | 2001 | |
NASA Design Reference Mission 3 1997 | 6 | 410 | 1997 | 2011 | |
NASA Mars Combo Lander 1998 | 4 | 280 | 1998 | 2011 | |
NASA Design Reference Mission 4 1998 | 6 | 400 | 1998 | 2011 | |
NASA Dual Lander Mission | 12 | 600 | 1999 | 2011 | |
Mars Society Mission 1999 | 10 | 900 | 1999 | 2011 | |
Marpost | 6 | 400 | 2000 | 2017 | |
Boeing Mars Transfer Vehicle & Lander Concepts for Human Exploration Missions in the 2031-2038 Time Frame | 6 | 100 | 2006 | 2038 | |
Mars Design Reference Mission 5 | 18 | 2009 | 2035 | ||
SpaceX Starship | 100 | 2012 | 2024 | ||
Inspiration Mars | 2 | 2013 | 2021 |