List of spacecraft powered by non-rechargeable batteries

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This is a list of spacecraft powered by non-rechargeable batteries. While most spacecraft are powered by longer-lasting power sources such as solar cells or radioisotope thermoelectric generators, which can provide power for years to decades, some have been powered by primary (non-rechargeable) electrochemical cells, which provide runtimes of minutes to months. This is typically done only on spacecraft that are planned to operate for only a short time, even if they must travel for a long time before being activated. Some spacecraft classes where this applies are atmospheric probes, short-duration landers, and technology demonstrators. Some early Earth satellites, such as the first Sputnik and Explorer satellites, also used primary batteries, before solar panels were widely adopted.

Contents

Uncrewed

Examples with non-rechargeable battery power only
Year [lower-alpha 1] SpacecraftRoleBattery life [lower-alpha 2] Type of BatteryParentNotes
1999 Deep Space 2 Scientific landers (2)1–3 days (planned) [1] Lithium–thionyl chloride [1] Mars Polar Lander Impact landers for Mars, lost during EDL
2016 ExoMars Schiaparelli Technology demonstration lander2–8 Martian sols (planned) [2] ExoMars Trace Gas Orbiter Lander for Mars, lost during EDL but considered a successful demo
1958 Explorer 1 Scientific satellite 111 days (actual)Zinc–mercury oxide (Zn–HgO) [3] Earth/space science [4]
1960 Explorer 8 Scientific satellite54 days (actual)Mercury [5] Earth science: ionospheric properties and micrometeorites
1966 Explorer 17 (AE-A)Scientific satellite98 days (actual)Earth science: upper atmospheric properties
1995 Galileo Probe Scientific atmospheric probe >57 or 78 minutes after entry (actual, due to overheating)[ citation needed ]

≥61.4 minutes after entry, 6 hours after waking up (planned) [6] [7]

Lithium–sulfur dioxide [8] [9]
Ca/CaCrO4 thermal (to fire pyrotechnics) [9]
Galileo Atmospheric entry into Jupiter
2004 [lower-alpha 3] Huygens Scientific atmospheric probe153 minutes or ≤3 hours (planned)[ citation needed ]Lithium–sulfur dioxide [10] Cassini Landed on Saturn's moon Titan
1959 Luna 1 Scientific lunar impactor (planned); scientific lunar flyby probe (actual)(closest lunar approach was 34 hours after launch)Silver–zinc, mercury oxide [11] Intended to crash into the Moon but missed. Performed lunar flyby instead. Now derelict in heliocentric orbit
1959 Luna 2 Scientific lunar impactor>1 day, 14 hours, 22 minutes, 42 seconds (actual, from launch to impact) [12] Succeeded in impacting the Moon, where Luna 1 had failed
1966 Luna 10 Scientific lunar orbiter219 transmissions over 460 orbits (actual)[ citation needed ]Studied radiation, fields, particles, meteorites, gravity [13]
1966 Luna 11 Scientific lunar orbiter137 transmissions over 277 orbits (actual)[ citation needed ]Lunar orbit [14]
1976 Luna 24 Scientific lunar lander with sample return [15]
2018 MASCOT Scientific rover >17 hours (actual)

<17 hours (planned) [16]

Hayabusa2 Hopping rover that landed on asteroid 162173 Ryugu
2022 Lunar Excursion Vehicle (LEV-1)Technology demonstration1-14 days (planned)Lunar surface rover, demonstration of crewed lunar vehicle's wheels
1972 Mars 2 and 3 landersScientific landers with tethered rovers (1 each)Mars 2 and 3 orbitersRovers were ski walking type and were not deployed due to lander failures [17]
1961 Mercury-Scout 1 Technical satellite18.5 hours (planned) [18] Launch failure [18]
1959 Pioneer 4 Scientific lunar flyby probe3 days, 10 hoursMercury [19] Derelict in heliocentric orbit
1978 Pioneer Venus Multiprobe Scientific atmospheric probes (1 large, 3 small)>54 minutes (Large Probe actual)

>53 minutes (North Probe actual)

123 minutes (Day Probe actual)

>56 minutes (Night Probe actual)

Silver–zinc (AgZn) [20] Pioneer Venus Bus Atmospheric entry into Venus. Day Probe survived impact and presumably died due to battery exhaustion. There was also a solar-powered bus that entered the atmosphere along with the probes
1989Phobos Hopper (Prop-F)Scientific lander3 hours (planned) Phobos 2 Hopping lander for Phobos. Phobos 2 was lost en route to Phobos due to computer failure
1957 Sputnik Technology demonstration satellite22 days/326 orbits (actual) [21] Silver–zinc (AgZn) [22] Earth satellite
2006 SuitSat-1 Technical/commemorative satellitebetween 2 orbits/~3 hours and 15 days (actual)[ citation needed ] ISS Earth satellite
1966–1969 Venera atmospheric probesScientific atmospheric probes>53 minutes (Venera 5 actual)

>51 minutes (Venera 6 actual)

Veneras 3–6 were atmospheric probes. Venera 3 failed upon entry. Venera 4 failed during descent due to overpressure. Veneras 5 and 6 were originally planned as landers, but changed to atmospheric probes due to learning about Venus's atmospheric pressure. Their parachutes were shrunk to increase descent speed, so as to reach crush depth before battery exhaustion
1970, 1972Venera 7 and 8 landersScientific landers58 minutes total (Venera 7 actual) [lower-alpha 4] [23] >50 minutes after landing (Venera 8 actual, until failure due to environmental conditions)

greater than up to 127 minutes (actual)

Venera 8–14 busesMost Venera landers' relay craft passed out of radio link range/geometry before the landers overheated or ran out of battery energy, rather than data return duration being limited by overheating as is commonly believed
1975–1982Venera 9 to 14 landersScientific landers>53 minutes after landing (Venera 9 actual)

>65 minutes after landing (Venera 10 actual)

>95 minutes after landing (Venera 11 actual)

>110 minutes after landing (Venera 12 actual)

>127 minutes after landing (Venera 13 actual)

>57 minutes after landing (Venera 14 actual)

30 minutes after landing (Venera 9–12 planned)

32 minutes after landing (Venera 13 and 14 planned)

1985Vega 1 and 2 landersScientific landers Vega 1 and 2 buses
1985Vega 1 and 2 balloonsScientific balloon aerobots 48–52 hours (expected) [24] Lithium [24]
2022SORA-Q Transformable Lunar Robot [25] Lunar rover Two hours [26] Lithium [27] Hakuto-R Mission 1 landerLost with Hakuto-R's failed landing.
2023 SLIM landerImaged SLIM lander on lunar surface.
  1. Year of battery-powered operation, if later than launch year
  2. From either launch or start of battery-powered operation to end of mission due to either battery failure or another cause. If the mission ended due to a cause other than battery failure, battery life is given as ">" (greater than) because the battery could have lasted longer.
  3. Launched 1997
  4. Venera 7 separated from its bus after atmospheric entry, at an altitude of 60 km. The parachute failed during descent, and the lander was knocked onto its side upon landing. This caused the radio link geometry to be suboptimal, reducing received signal strength and the duration a given received signal strength could be maintained. It was a few weeks after the landing that it was discovered from analyzing recordings of the received signal that the lander had kept transmitting after landing, but the signal was received too weakly to discern at first.
Examples with a supplementary power
WhatParentType of BatterySecondaryNotes
Luna 9 Solar [28] Lunar landing (1966)
Sojourner rover Mars Pathfinder Lithium-thionyl chloride (LiSOCL2) [29] SolarRoved Mars (1997)
Sputnik 3 -Silver-Zinc [30] Solar (Experiment)Earth satellite
Philae Rosetta Lithium-thionyl chloride (LiSOCl2) (900 W*h)
Lithiu-ion (Li-ion) (100 W*h)
SolarComet 67P/Churyumov–Gerasimenko (2014) [31]
Vanguard 1 Mercury [32] Earth satellite (1958)

Primary power comes from a chemical battery, but a secondary system exists. For example, Luna 9 ran out of power after three days. [28]


Crewed

See also

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