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Progress (spacecraft)

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Progress
Progress MS-11 spacecraft in space
Country of originSoviet Union / Russia
OperatorRoscosmos
Applications
  • Cargo resupply
Specifications
Spacecraft typeCargo
Payload capacity2,400 kg (5,300 lb)
Volume7.6 m3 (270 cu ft)
Design life180 days docked to a space station[a]
Dimensions
Length7.23 m (23.7 ft)
Diameter2.72 m (8 ft 11 in)
Production
Built182
Lost2

The Progress (Russian: Прогресс) is a Russian expendable cargo spacecraft. Originally developed for the Soviet space program and derived from the crewed Soyuz spacecraft, Progress has been instrumental in maintaining long-duration space missions by providing consumables like food, water, and air, as well as maintenance equipment. Since its maiden flight in 1978, Progress has supported various space stations, including Salyut 6, Salyut 7, and Mir, and remains a key resupply vehicle for the International Space Station (ISS).

Each Progress mission delivers thousands of kilograms of supplies in its pressurized module. It also carries water, fuel, and gases to replenish the station's resources and sustain its onboard atmosphere. Beyond resupply duties, a docked Progress can maneuver or reboost the station, countering atmospheric drag and maintaining its operational altitude. When a Progress spacecraft nears the end of its design life, it is loaded with waste, undocked, and deorbited to safely disintegrate in Earth's atmosphere.

As of November 2024, there have been 182 Progress flights, with only three failures, all occurring between 2011 and 2016. Typically, three to four Progress flights are launched to the ISS each year. Due to the variation in Progress vehicles flown to the ISS, NASA uses its own nomenclature where "ISS 1P" means the first Progress spacecraft to ISS.

Design

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The Progress spacecraft shares much of design with the crewed Soyuz spacecraft but with several modifications to make it better suited to cargo transport. It consists of three distinct sections:[1]

  • Cargo Section: This pressurized carries supplies for the crew, including maintenance items, prepackaged and fresh food, scientific equipment, and clothing. Its docking drogue, similar to that of the Soyuz, features ducting that enables fuel transfer (described below).
  • Tanker Section: Replacing the Soyuz’s reentry module, this unpressurized compartment houses two tanks containing unsymmetrical dimethylhydrazine (UDMH) fuel and dinitrogen tetroxide (N2O4) oxidizer. Ducts run from these tanks around the outside of the pressurized module to connectors at the docking port, allowing automated fuel transfer. This design prevents any potential leaks of the toxic propellant from contaminating the station's atmosphere. This section also contains water tanks.
  • Propulsion Section: Located at the rear of the spacecraft, this unpressurized compartment remains largely unchanged from the Soyuz design. It contains the orientation engines used for automatic docking and can be utilized to boost the station's orbit once docked.

The Progress spacecraft’s uncrewed and disposable design enables significant weight reduction. Unlike Soyuz, it does not require life support systems, heat shields, parachutes, or automatic crew rescue systems. Additionally, it lacks the ability to separate into multiple modules. After completing its mission, the spacecraft undocks, performs a controlled retrofire, and burns up upon reentry into Earth's atmosphere.

Versions

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There were many small variations between the different flights, but the major upgrades are reflected in the change of name.

Progress (1978–1990)

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Progress logistics resupply spacecraft. It consists of the dry cargo module (left); the tanker compartment (center); and a stretched service module (right).

There were 42 spacecraft built using the initial Progress design, the last one being launched in May 1990.

The bureau in charge of designing the freighter was TsKBEM (now RKK Energia). They began work on the design in mid-1973, assigning Progress the GRAU index 11F615A15. The design was complete by February 1974, and the first production model was ready for launch in November 1977. Progress 1 launched on 20 January 1978 aboard the same rocket used to launch the Soyuz. It still featured the same launch shroud as the Soyuz, though this was purely for aerodynamic purposes as the launch escape system had been deactivated.

This first version of Progress had a mass of 7,020 kg (15,480 lb) and carried 2,300 kg (5,100 lb) of cargo, or 30% of its launch mass. It had the same diameter as the Soyuz at 2.2 m (7 ft 3 in), but was 8 m (26 ft) in length – slightly longer. The autonomous flight time was 3 days, the same time as that of the Soyuz ferry. It could spend 30 days docked. Progress always docked to the aft port of the station it was resupplying (the aft being where the main rocket engines of the station and their tankage, for refueling by the Progress, are located).

  • Launch mass: 7,020–7,249 kg (15,476–15,981 lb)
  • Mass of cargo:
    • ~2,300 kg (5,100 lb) (before Progress-24)
    • ~2,500 kg (5,500 lb) (from Progress-24)
  • Length: 7.94 m (26.0 ft)
  • Diameter of cargo modules: 2.2 m (7 ft 3 in)
  • Maximum diameter: 2.72 m (8 ft 11 in)
  • Volume of cargo compartment: 6.6 m3 (230 cu ft)

Progress-M 11F615A55 (1989–2021)

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Diagram of exterior of the Progress-M logistics resupply spacecraft
Diagram of interior of the Progress-M spacecraft

The upgraded Progress M (GRAU: 11F615A55, manufacturer's designation: 7K-TGM) was first launched in August 1989. The first 43 flights all went to Mir; following Mir's re-entry, Progress was used as the resupply vehicle for the International Space Station. As of December 2020, there have been over 80 flights (over different configurations) to the ISS and more are scheduled.[2]

The Progress M is essentially the same spacecraft as the Progress, but it features improvements based on the Soyuz-T and Soyuz-TM designs. It can spend up to 30 days in autonomous flight and is able to carry 100 kg (220 lb) more. Also, unlike the old Progress crafts, it can return items to Earth. This is accomplished by using the VBK-Raduga capsule, which can carry up to 150 kg (330 lb) of cargo. It is 1.5 m (4 ft 11 in) long and 60 cm (24 in) in diameter and has a "dry mass" of 350 kg (770 lb). Progress M can also dock to the forward port of the station and still transfer fuel. It uses the same rendezvous system as the Soyuz, and it features solar panels for the first time. The last launch was of Progress M-UM on 24 November 2021.

  • Launch mass: 7,130 kg (15,720 lb)
  • Cargo mass: 2,600 kg (5,700 lb)
  • Dry cargo mass: 1,500 kg (3,300 lb)
  • Liquid cargo mass: 1,540 kg (3,400 lb)
  • Length: 7.23 m (23.7 ft)
  • Diameter of cargo modules: 2.2 m (7 ft 3 in)
  • Maximum diameter: 2.72 m (8 ft 11 in)
  • Dry cargo compartment volume: 7.6 m3 (270 cu ft)
  • Solar array span: 10.6 m (35 ft)

Progress-М 11F615A60 (2008–2015)

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A new modification of the Progress spacecraft, with new TsVM-101 digital flight computer and MBITS digital telemetry system,[3] was first launched on 26 November 2008, at 12:38 UTC from the Kazakhstan's Baikonur Cosmodrome spaceport aboard a Russian Soyuz rocket. The first spacecraft of this series was Progress M-01M.

The spacecraft belongs to the so-called 400 series (GRAU: 11F615A60), and all modifications applied to it were subsequently used in the production of new Soyuz TMA-01M[4] crewed spacecraft.

Progress M-27M was launched on 28 April 2015, but communication with the vessel was lost soon after, and it was destroyed as it re-entered the atmosphere on 8 May 2015.[5] The last launch was Progress M-29M.

Progress M1 (2000–2004)

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Progress M1 is another variant, capable of carrying more propellant (but less total cargo) to the space station. There have been 11 of these flights.

  • Mass: 7,150 kg (15,760 lb)
  • Capacity cargo: 2,230 kg (4,920 lb)
  • Capacity dry cargo: 1,800 kg (4,000 lb)
  • Capacity propellant: 1,950 kg (4,300 lb)

Progress M2

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Progress M2 was a planned variant, which was a proposed design for the proposed Mir-2 space station, but was dropped due to financial issues. The M2 variant would have a larger service module for larger cargo or space station modules and would have been launched on a Zenit rocket as the spacecraft is bigger.

Progress MS (2015–present)

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Progress MS is an improved variant which first launched on 21 December 2015. It has the following improvements:[6][7][8][9]

  • New external compartment that enables it to deploy satellites. Each compartment can hold up to four launch containers. First time installed on Progress MS-03.
  • Enhanced redundancy thanks to the addition of a backup system of electrical motors for the docking and sealing mechanism.
  • Improved micrometeoroid protection with additional panels in the cargo compartment.
  • Luch relay satellite link capabilities enable telemetry and control even when not in direct view of ground radio stations.
  • GNSS autonomous navigation enables real time determination of the status vector and orbital parameters dispensing with the need of ground station orbit determination.
  • Real time relative navigation thanks to direct radio data exchange capabilities with the space station.
  • New digital radio that enables enhanced TV camera view for the docking operations.
  • Unified Command Telemetry System replaces previous Chezara Kvant-V as the Progress spacecraft's on-board radio and antenna/feeder system.
  • Replacement of the Kurs A with Kurs NA digital system.

Current status

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Progress spacecraft are used to resupply the International Space Station (ISS) as of 2021. Between 1 February 2003 and 26 July 2005, they were the only spacecraft available to transport large quantities of supplies to the station, as the Space Shuttle fleet was grounded after the breakup of Columbia at the end of STS-107. For ISS missions, the Progress M1 variant is used, which moves the water tanks from the propellant and refueling module to the pressurized section, and as a result is able to carry more propellant. Progress M-UM, the final flight of a Progress-M spacecraft, was launched 24 November 2021 on a Soyuz 2.1b. As of 7/1/2021, there have been 170 Progress flights to the ISS.

On 9 July 2018, Progress MS-09 broke a previous record by reaching the ISS in 3 hours and 48 minutes, carrying about 2,450 kg (5,400 lb) of cargo and supplies. It delivered food, fuel and supplies, including 705 kg of propellant, 50 kg (110 lb) of oxygen and air, 420 kg (930 lb) of water.

The European Space Agency (ESA) operated its own type of robotic supply freighter, the Automated Transfer Vehicle (ATV). The first of these, named Jules Verne, was launched at 04:03 UTC on 9 March 2008. ATVs can carry up to 8.85 tonnes of cargo into space, roughly three times as much as the Progress, and were launched annually by Ariane 5 rockets from 2011-2014 as part of ESA contribution to ISS upkeep. The design is adopted as the Service Module of the Orion spacecraft.

NASA's planned Orion spacecraft was initially designed to have an uncrewed variant of the Crew module similar to Progress; however, this capability was removed in 2009.[10] As of 2023, SpaceX's Dragon spacecraft and Northrop Grumman's Cygnus spacecraft handle American logistics to the International Space Station.

See also

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Notes

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  1. ^ Progress MS-14 remained docked more than one year

References

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  1. ^ "Progress cargo ship". www.russianspaceweb.com. Retrieved 23 November 2024.
  2. ^ "NASA Launch Schedule and NASA". Public Domain This article incorporates text from this source, which is in the public domain.
  3. ^ Krebs, Gunter. "Progress M-01M – 25M (11F615A60, 7KTGM)". Gunter's Space Page. Retrieved 29 March 2013.
  4. ^ Krebs, Gunter. "Soyuz-TMA 01M – 16M (7K-STMA, 11F747)". Gunter's Space Page. Retrieved 29 March 2013.
  5. ^ "РОСКОСМОС: ТГК "ПРОГРЕСС М-27М" ПРЕКРАТИЛ СУЩЕСТВОВАНИЕ". Federal Space. 8 May 2015. Archived from the original on 8 May 2015. Retrieved 15 December 2015.
  6. ^ "Upgraded Progress Transport Cargo Spacecraft Getting Ready for Launch". Yuzhny Space Center. 10 August 2015. Archived from the original on 4 March 2016. Retrieved 13 August 2015.
  7. ^ Krebs, Gunter (1 December 2015). "Progress-MS 01-19". Gunter's Space Page. Retrieved 16 November 2018.
  8. ^ Zak, Anatoly (16 November 2018). "Progress-MS". RussianSpaceWeb.com. Retrieved 4 June 2019.
  9. ^ Blau, Patrick. "Progress MS Spacecraft". Spaceflight101.com. Retrieved 17 November 2020.
  10. ^ Chris Bergin (4 July 2009). "Constellation battle numerous Top Risks – Orion loses unmanned capability". NASASpaceFlight.com. Retrieved 29 March 2013.
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