Jump to content

Uncrewed spacecraft

From Wikipedia, the free encyclopedia
(Redirected from Unmanned space mission)

The uncrewed resupply vessel Progress M-06M
Galileo space probe, prior to departure from Earth orbit in 1989
Uncrewed spacecraft Buran launched, orbited Earth, and landed as an uncrewed spacecraft in 1988 (shown here at an airshow)
Model of James Webb Space Telescope
Top: The uncrewed resupply vessel Progress M-06M (left). Galileo space probe, prior to departure from Earth orbit in 1989 (right).
Bottom: Spaceplane Buran was launched, orbited Earth, and landed as an uncrewed spacecraft in 1988 (left). Model of James Webb Space Telescope (right).

Uncrewed spacecraft or robotic spacecraft are spacecraft without people on board. Uncrewed spacecraft may have varying levels of autonomy from human input, such as remote control, or remote guidance. They may also be autonomous, in which they have a pre-programmed list of operations that will be executed unless otherwise instructed. A robotic spacecraft for scientific measurements is often called a space probe or space observatory.

Many space missions are more suited to telerobotic rather than crewed operation, due to lower cost and risk factors. In addition, some planetary destinations such as Venus or the vicinity of Jupiter are too hostile for human survival, given current technology. Outer planets such as Saturn, Uranus, and Neptune are too distant to reach with current crewed spaceflight technology, so telerobotic probes are the only way to explore them. Telerobotics also allows exploration of regions that are vulnerable to contamination by Earth micro-organisms since spacecraft can be sterilized. Humans can not be sterilized in the same way as a spaceship, as they coexist with numerous micro-organisms, and these micro-organisms are also hard to contain within a spaceship or spacesuit.

The first uncrewed space mission was Sputnik, launched October 4, 1957 to orbit the Earth. Nearly all satellites, landers and rovers are robotic spacecraft. Not every uncrewed spacecraft is a robotic spacecraft; for example, a reflector ball is a non-robotic uncrewed spacecraft. Space missions where other animals but no humans are on-board are called uncrewed missions.

Many habitable spacecraft also have varying levels of robotic features. For example, the space stations Salyut 7 and Mir, and the International Space Station module Zarya, were capable of remote guided station-keeping and docking maneuvers with both resupply craft and new modules. Uncrewed resupply spacecraft are increasingly used for crewed space stations.


A replica of Sputnik 1 at the U.S. National Air and Space Museum
A replica of Explorer 1

The first robotic spacecraft was launched by the Soviet Union (USSR) on 22 July 1951, a suborbital flight carrying two dogs Dezik and Tsygan.[1] Four other such flights were made through the fall of 1951.

The first artificial satellite, Sputnik 1, was put into a 215-by-939-kilometer (116 by 507 nmi) Earth orbit by the USSR on 4 October 1957. On 3 November 1957, the USSR orbited Sputnik 2. Weighing 113 kilograms (249 lb), Sputnik 2 carried the first animal into orbit, the dog Laika.[2] Since the satellite was not designed to detach from its launch vehicle's upper stage, the total mass in orbit was 508.3 kilograms (1,121 lb).[3]

In a close race with the Soviets, the United States launched its first artificial satellite, Explorer 1, into a 357-by-2,543-kilometre (193 by 1,373 nmi) orbit on 31 January 1958. Explorer I was an 205-centimetre (80.75 in) long by 15.2-centimetre (6.00 in) diameter cylinder weighing 14.0 kilograms (30.8 lb), compared to Sputnik 1, a 58-centimeter (23 in) sphere which weighed 83.6 kilograms (184 lb). Explorer 1 carried sensors which confirmed the existence of the Van Allen belts, a major scientific discovery at the time, while Sputnik 1 carried no scientific sensors. On 17 March 1958, the US orbited its second satellite, Vanguard 1, which was about the size of a grapefruit, and which remains in a 670-by-3,850-kilometre (360 by 2,080 nmi) orbit as of 2016.

The first attempted lunar probe was the Luna E-1 No.1, launched on 23 September 1958. The goal of a lunar probe repeatedly failed until 4 January 1959 when Luna 1 orbited around the Moon and then the Sun.

The success of these early missions began a race between the US and the USSR to outdo each other with increasingly ambitious probes. Mariner 2 was the first probe to study another planet, revealing Venus' extremely hot temperature to scientists in 1962, while the Soviet Venera 4 was the first atmospheric probe to study Venus. Mariner 4's 1965 Mars flyby snapped the first images of its cratered surface, which the Soviets responded to a few months later with images from on its surface from Luna 9. In 1967, America's Surveyor 3 gathered information about the Moon's surface that would prove crucial to the Apollo 11 mission that landed humans on the Moon two years later.[4]

The first interstellar probe was Voyager 1, launched 5 September 1977. It entered interstellar space on 25 August 2012,[5] followed by its twin Voyager 2 on 5 November 2018.[6]

Nine other countries have successfully launched satellites using their own launch vehicles: France (1965),[7] Japan[8] and China (1970),[9] the United Kingdom (1971),[10] India (1980),[11] Israel (1988),[12] Iran (2009),[13] North Korea (2012),[14] and South Korea (2022).[15]


In spacecraft design, the United States Air Force considers a vehicle to consist of the mission payload and the bus (or platform). The bus provides physical structure, thermal control, electrical power, attitude control and telemetry, tracking and commanding.[16]


JPL divides the "flight system" of a spacecraft into subsystems.[17] These include:


An illustration's of NASA's planned Orion spacecraft approaching a robotic asteroid capture vehicle

The physical backbone structure, which

  • provides overall mechanical integrity of the spacecraft
  • ensures spacecraft components are supported and can withstand launch loads

Data handling[edit]

This is sometimes referred to as the command and data subsystem. It is often responsible for:

  • command sequence storage
  • maintaining the spacecraft clock
  • collecting and reporting spacecraft telemetry data (e.g. spacecraft health)
  • collecting and reporting mission data (e.g. photographic images)

Attitude determination and control[edit]

This system is mainly responsible for the correct spacecraft's orientation in space (attitude) despite external disturbance-gravity gradient effects, magnetic-field torques, solar radiation and aerodynamic drag; in addition it may be required to reposition movable parts, such as antennas and solar arrays.[18]

Entry, descent, and landing[edit]

Integrated sensing incorporates an image transformation algorithm to interpret the immediate imagery land data, perform a real-time detection and avoidance of terrain hazards that may impede safe landing, and increase the accuracy of landing at a desired site of interest using landmark localization techniques. Integrated sensing completes these tasks by relying on pre-recorded information and cameras to understand its location and determine its position and whether it is correct or needs to make any corrections (localization). The cameras are also used to detect any possible hazards whether it is increased fuel consumption or it is a physical hazard such as a poor landing spot in a crater or cliff side that would make landing very not ideal (hazard assessment).

Landing on hazardous terrain[edit]

In planetary exploration missions involving robotic spacecraft, there are three key parts in the processes of landing on the surface of the planet to ensure a safe and successful landing.[19] This process includes an entry into the planetary gravity field and atmosphere, a descent through that atmosphere towards an intended/targeted region of scientific value, and a safe landing that guarantees the integrity of the instrumentation on the craft is preserved. While the robotic spacecraft is going through those parts, it must also be capable of estimating its position compared to the surface in order to ensure reliable control of itself and its ability to maneuver well. The robotic spacecraft must also efficiently perform hazard assessment and trajectory adjustments in real time to avoid hazards. To achieve this, the robotic spacecraft requires accurate knowledge of where the spacecraft is located relative to the surface (localization), what may pose as hazards from the terrain (hazard assessment), and where the spacecraft should presently be headed (hazard avoidance). Without the capability for operations for localization, hazard assessment, and avoidance, the robotic spacecraft becomes unsafe and can easily enter dangerous situations such as surface collisions, undesirable fuel consumption levels, and/or unsafe maneuvers.


Components in the telecommunications subsystem include radio antennas, transmitters and receivers. These may be used to communicate with ground stations on Earth, or with other spacecraft.[20]

Electrical power[edit]

The supply of electric power on spacecraft generally come from photovoltaic (solar) cells or from a radioisotope thermoelectric generator. Other components of the subsystem include batteries for storing power and distribution circuitry that connects components to the power sources.[21]

Temperature control and protection from the environment[edit]

Spacecraft are often protected from temperature fluctuations with insulation. Some spacecraft use mirrors and sunshades for additional protection from solar heating. They also often need shielding from micrometeoroids and orbital debris.[22]


Spacecraft propulsion is a method that allows a spacecraft to travel through space by generating thrust to push it forward.[23] However, there is not one universally used propulsion system: monopropellant, bipropellant, ion propulsion, etc. Each propulsion system generates thrust in slightly different ways with each system having its own advantages and disadvantages. But, most spacecraft propulsion today is based on rocket engines. The general idea behind rocket engines is that when an oxidizer meets the fuel source, there is explosive release of energy and heat at high speeds, which propels the spacecraft forward. This happens due to one basic principle known as Newton's Third Law. According to Newton, "to every action there is an equal and opposite reaction." As the energy and heat is being released from the back of the spacecraft, gas particles are being pushed around to allow the spacecraft to propel forward. The main reason behind the usage of rocket engine today is because rockets are the most powerful form of propulsion there is.


For a propulsion system to work, there is usually an oxidizer line and a fuel line. This way, the spacecraft propulsion is controlled. But in a monopropellant propulsion, there is no need for an oxidizer line and only requires the fuel line.[24] This works due to the oxidizer being chemically bonded into the fuel molecule itself. But for the propulsion system to be controlled, the combustion of the fuel can only occur due to a presence of a catalyst. This is quite advantageous due to making the rocket engine lighter and cheaper, easy to control, and more reliable. But, the downfall is that the chemical is very dangerous to manufacture, store, and transport.


A bipropellant propulsion system is a rocket engine that uses a liquid propellent.[25] This means both the oxidizer and fuel line are in liquid states. This system is unique because it requires no ignition system, the two liquids would spontaneously combust as soon as they come into contact with each other and produces the propulsion to push the spacecraft forward. The main benefit for having this technology is because that these kinds of liquids have relatively high density, which allows the volume of the propellent tank to be small, therefore increasing space efficacy. The downside is the same as that of monopropellant propulsion system: very dangerous to manufacture, store, and transport.


An ion propulsion system is a type of engine that generates thrust by the means of electron bombardment or the acceleration of ions.[26] By shooting high-energy electrons to a propellant atom (neutrally charge), it removes electrons from the propellant atom and this results the propellant atom becoming a positively charged atom. The positively charged ions are guided to pass through positively charged grids that contains thousands of precise aligned holes are running at high voltages. Then, the aligned positively charged ions accelerates through a negative charged accelerator grid that further increases the speed of the ions up to 40 kilometres per second (90,000 mph). The momentum of these positively charged ions provides the thrust to propel the spacecraft forward. The advantage of having this kind of propulsion is that it is incredibly efficient in maintaining constant velocity, which is needed for deep-space travel. However, the amount of thrust produced is extremely low and that it needs a lot of electrical power to operate.

Mechanical devices[edit]

Mechanical components often need to be moved for deployment after launch or prior to landing. In addition to the use of motors, many one-time movements are controlled by pyrotechnic devices.[27]

Robotic vs. uncrewed spacecraft[edit]

Robotic spacecraft are specifically designed system for a specific hostile environment.[28] Due to their specification for a particular environment, it varies greatly in complexity and capabilities. While an uncrewed spacecraft is a spacecraft without personnel or crew and is operated by automatic (proceeds with an action without human intervention) or remote control (with human intervention). The term 'uncrewed spacecraft' does not imply that the spacecraft is robotic.


Robotic spacecraft use telemetry to radio back to Earth acquired data and vehicle status information. Although generally referred to as "remotely controlled" or "telerobotic", the earliest orbital spacecraft – such as Sputnik 1 and Explorer 1 – did not receive control signals from Earth. Soon after these first spacecraft, command systems were developed to allow remote control from the ground. Increased autonomy is important for distant probes where the light travel time prevents rapid decision and control from Earth. Newer probes such as Cassini–Huygens and the Mars Exploration Rovers are highly autonomous and use on-board computers to operate independently for extended periods of time.[29][30]

Space probes and observatories[edit]

A space probe is a robotic spacecraft that does not orbit Earth, but instead, explores further into outer space. Space probes have different sets of scientific instruments onboard. A space probe may approach the Moon; travel through interplanetary space; flyby, orbit, or land on other planetary bodies; or enter interstellar space. Space probes send collected data to Earth. Space probes can be orbiters, landers, and rovers. Space probes can also gather materials from its target and return it to Earth.[31][32]

Once a probe has left the vicinity of Earth, its trajectory will likely take it along an orbit around the Sun similar to the Earth's orbit. To reach another planet, the simplest practical method is a Hohmann transfer orbit. More complex techniques, such as gravitational slingshots, can be more fuel-efficient, though they may require the probe to spend more time in transit. Some high Delta-V missions (such as those with high inclination changes) can only be performed, within the limits of modern propulsion, using gravitational slingshots. A technique using very little propulsion, but requiring a considerable amount of time, is to follow a trajectory on the Interplanetary Transport Network.[33]

A space telescope or space observatory is a telescope in outer space used to observe astronomical objects. Space telescopes avoid the filtering and distortion of electromagnetic radiation which they observe, and avoid light pollution which ground-based observatories encounter. They are divided into two types: satellites which map the entire sky (astronomical survey), and satellites which focus on selected astronomical objects or parts of the sky and beyond. Space telescopes are distinct from Earth imaging satellites, which point toward Earth for satellite imaging, applied for weather analysis, espionage, and other types of information gathering.

Cargo spacecraft[edit]

A collage of automated cargo spacecraft used in the past or present to resupply the International Space Station

Cargo or resupply spacecraft are robotic spacecraft that are designed specifically to carry cargo, possibly to support space stations' operation by transporting food, propellant and other supplies. This is different from a space probe, whose missions are to conduct scientific investigations.

Automated cargo spacecraft have been used since 1978 and have serviced Salyut 6, Salyut 7, Mir, the International Space Station and Tiangong space station.

As of 2024, four different cargo spacecraft are used to supply the International Space Station: Russian Progress, [34] American SpaceX Dragon 2,[35][36] Cygnus, [37] and Dream Chaser.[38][39] Chinese Tianzhou is used to supply Tiangong space station.[40][41][42]

See also[edit]


  1. ^ Asif Siddiqi, Sputnik and the Soviet Space Challenge, University Press of Florida, 2003, ISBN 081302627X, p. 96
  2. ^ Whitehouse, David (28 October 2002). "First dog in space died within hours". BBC News World Edition. Archived from the original on 17 July 2013. Retrieved 10 May 2013. The animal, launched on a one-way trip on board Sputnik 2 in November 1957, was said to have died painlessly in orbit about a week after blast-off. Now, it has been revealed she died from overheating and panic just a few hours after the mission started.
  3. ^ "Sputnik 2, Russian Space Web". 3 November 2012. Archived from the original on 2 February 2023. Retrieved 7 January 2023.
  4. ^ "NASA - What Is a Space Probe?". www.nasa.gov. Archived from the original on 30 August 2021. Retrieved 9 January 2023.
  5. ^ Barnes, Brooks (12 September 2013). "In a Breathtaking First, NASA's Voyager 1 Exits the Solar System". The New York Times. ISSN 0362-4331. Archived from the original on 7 April 2019. Retrieved 1 August 2022.
  6. ^ Potter, Sean (9 December 2018). "NASA's Voyager 2 Probe Enters Interstellar Space". NASA. Archived from the original on 21 May 2022. Retrieved 1 August 2022.
  7. ^ "France launches first satellite". UPI. 26 November 1965. Retrieved 4 March 2023.
  8. ^ "11 February 1970. This Day in History: Japan launches its first satellite". History Channel. Archived from the original on 5 March 2023. Retrieved 4 March 2023.
  9. ^ "Timeline: Major milestones in Chinese space exploration". Reuters. 22 November 2020. Archived from the original on 5 March 2023. Retrieved 4 March 2023.
  10. ^ Ben Judge (28 October 2020). "28 October 1971: Britain's only independent satellite launch". Money Week. Archived from the original on 5 March 2023. Retrieved 4 March 2023.
  11. ^ VP Sandlas (31 August 2018). "Blast from the past: An insider's account of India's first successful experimental satellite launch". Archived from the original on 8 November 2023. Retrieved 4 March 2023.
  12. ^ Glenn Frankel (20 September 1988). "Israel Launches its First Satellite into Orbit". Washington Post. Archived from the original on 8 November 2023. Retrieved 4 March 2023.
  13. ^ "Iran launches first satellite, draws concern". Los Angeles Times. 3 February 2009. Archived from the original on 5 March 2023. Retrieved 4 March 2023.
  14. ^ "North Korea Launches First Satellite into Orbit". Space News. 14 December 2012. Archived from the original on 8 November 2023. Retrieved 4 March 2023.
  15. ^ "South Korea launches first satellite with homegrown rocket". NBC News. 22 June 2022. Archived from the original on 8 November 2023. Retrieved 5 March 2023.
  16. ^ "Air University Space Primer, Chapter 10 – Spacecraft Design, Structure And Operation" (PDF). USAF. Archived from the original (PDF) on 21 December 2016. Retrieved 13 October 2007.
  17. ^ "Chapter 11. Typical Onboard Systems". JPL. Archived from the original on 28 April 2015. Retrieved 10 June 2008.
  18. ^ Wiley J. Larson; James R. Wertz(1999). Space Mission Analysis and Design, 3rd ed. Microcosm. pp. 354. ISBN 978-1-881883-10-4,
  19. ^ Howard, Ayanna (January 2011). "Rethinking public–private space travel". Space Policy. 29 (4): 266–271. Bibcode:2013SpPol..29..266A. doi:10.1016/j.spacepol.2013.08.002.
  20. ^ LU. K. Khodarev (1979). "Space Communications". The Great Soviet Encyclopedia. Archived from the original on 10 May 2013. Retrieved 10 May 2013. The transmission of information between the earth and spacecraft, between two or more points on the earth via spacecraft or using artificial means located in space (a belt of needles, a cloud of ionized particles, and so on), and between two or more spacecraft.
  21. ^ Wiley J. Larson; James R. Wertz (1999). Space Mission Analysis and Design, 3rd ed.. Microcosm. pp. 409. ISBN 978-1-881883-10-4,
  22. ^ "Micrometeoroid and Orbital Debris (MMOD) Protection" (PDF). NASA. Archived from the original (PDF) on 29 October 2009. Retrieved 10 May 2013.
  23. ^ Hall, Nancy (5 May 2015). "Welcome to the Beginner's Guide to Propulsion". NASA. Archived from the original on 8 November 2023. Retrieved 7 January 2023.
  24. ^ Zhang, Bin (October 2014). "A verification framework with application to a propulsion system". Expert Systems with Applications. 41 (13): 5669–5679. doi:10.1016/j.eswa.2014.03.017.
  25. ^ Chen, Yang (April 2017). "Dynamic modeling and simulation of an integral bipropellant propulsion double-valve combined test system" (PDF). Acta Astronautica. 133: 346–374. Bibcode:2017AcAau.133..346C. doi:10.1016/j.actaastro.2016.10.010. Archived from the original on 8 November 2023. Retrieved 7 January 2023.
  26. ^ Patterson, Michael (August 2017). "Ion Propulsion". NASA. Archived from the original on 31 December 2018. Retrieved 7 January 2023.
  27. ^ Wiley J. Larson; James R. Wertz(1999). Space Mission Analysis and Design, 3rd ed. Microcosm. pp. 460. ISBN 978-1-881883-10-4,
  28. ^ Davis, Phillips. "Basics of Space Flight". NASA. Archived from the original on 2 June 2019. Retrieved 7 January 2023.
  29. ^ K. Schilling; W. Flury (11 April 1989). "AUTONOMY AND ON-BOARD MISSION MANAGEMENT ASPECTS FOR THE CASSINI-TITAN PROBE". ATHENA MARS EXPLORATION ROVERS. Archived from the original (PDF) on 5 May 2013. Retrieved 10 May 2013. Current space missions exhibit a rapid growth in the requirements for on-board autonomy. This is the result of increases in mission complexity, intensity of mission activity and mission duration. In addition, for interplanetary spacecraft, the operations are characterized by complicated ground control access, due to the large distances and the relevant solar system environment[…] To handle these problemsn, the spacecraft design has to include some form of autonomous control capability.
  30. ^ "Frequently Asked Questions (Athena for kids): Q) Is the rover controlled by itself or controlled by scientists on Earth?" (PDF). ATHENA MARS EXPLORATION ROVERS. 2005. Archived from the original (PDF) on 29 October 2009. Retrieved 10 May 2013. Communication with Earth is only twice per sol (martian day) so the rover is on its own (autonomous) for much of its journey across the martian landscape. Scientists send commands to the rover in a morning "uplink" and gather data in an afternoon "downlink." During an uplink, the rover is told where to go, but not exactly how to get there. Instead, the command contains the coordinates of waypoints toward a desired destination. The rover must navigate from waypoint to waypoint without human help. The rover has to use its "brain" and its "eyes" for these instances. The "brain" of each rover is the onboard computer software that tells the rover how to navigate based on what the Hazcams (hazard avoidance cameras) see. It is programmed with a given set of responses to a given set of circumstances. This is called "autonomy and hazard avoidance."
  31. ^ "NASA - What Is a Space Probe?". www.nasa.gov. Archived from the original on 30 August 2021. Retrieved 26 February 2023.
  32. ^ "Space Probes". education.nationalgeographic.org. Archived from the original on 26 February 2023. Retrieved 26 February 2023.
  33. ^ Ross, S. D. (2006). "The Interplanetary Transport Network" (PDF). American Scientist. 94 (3): 230–237. doi:10.1511/2006.59.994. Archived (PDF) from the original on 20 October 2013. Retrieved 27 June 2013.
  34. ^ Abbey A. Donaldson (12 February 2024). "NASA to Provide Coverage of Progress 87 Launch, Space Station Docking". Nasa.
  35. ^ Post, Hannah (16 September 2014). "NASA Selects SpaceX to be Part of America's Human Spaceflight Program". SpaceX. Archived from the original on 15 March 2019. Retrieved 3 March 2019.
  36. ^ Berger, Eric (9 June 2017). "So SpaceX is having quite a year". Ars Technica. Archived from the original on 9 June 2017. Retrieved 9 June 2017.
  37. ^ Jeff Foust (30 January 2024). "Falcon 9 launches Cygnus cargo spacecraft to space station". Space News.
  38. ^ "SNC Selects ULA for Dream Chaser® Spacecraft Launches". Sierra Nevada Corporation (Press release). 14 August 2019. Retrieved 14 August 2019.
  39. ^ "NASA Deputy Administrator Lori Garver touts Colorado's role". Youtube.com. 5 February 2011. Retrieved 29 August 2012.
  40. ^ "长征七号遥三火箭 • 天舟二号货运飞船 • LongMarch-7 Y3 • Tianzhou-2". spaceflightfans.cn (in Chinese). 21 April 2021. Archived from the original on 11 June 2021. Retrieved 25 May 2021.
  41. ^ Jones, Andrew (13 April 2021). "China preparing Tianzhou-2 cargo mission to follow upcoming space station launch". SpaceNews. Retrieved 24 April 2021.
  42. ^ "China rolls out rocket for Tianzhou 3 cargo mission ahead of Monday launch (Photos)". Space.com. 17 September 2021.