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Progress-M1 - Wikipedia

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Progress-M1
Specifications
A Progress-M1 spacecraft

Manufacturer	RKK Energia
Country of origin	Russia
Operator	Roskosmos
Applications	Space station logistics


Regime	Low Earth
Design life	6 months



Production
Status	Retired
Built	11F615A55: 11 11F615A70: 0
Launched	11F615A55: 11 11F615A60: 0
Retired	11F615A55: 11
Maiden launch	11F615A55: Progress M1-1 (2000) 11F615A70: Progress M1-01M (2011) (cancelled)
Last launch	11F615A55: Progress M1-11 (2004)
Last retirement	11F615A55: Progress M1-11 (2004)


Related spacecraft
Derived from	Progress-M

Progress-M1 (Russian: Прогресс-М1, GRAU indices 11F615A55 and 11F615A70), also known as Progress 7K-TGM1, is a Russian spacecraft which is used to resupply space stations. It is a variant of the Progress spacecraft, derived from the Progress-M, but modified to carry more UDMH and N₂O₄ propellant for refuelling the International Space Station instead of other cargoes such as water. A Progress M1 11F615A55 spacecraft could carry up to 1,700 kilograms (3,700 lb) of propellant in eight mid-section refuelling tanks,^[1] compared to the 850 kilograms (1,870 lb) that a Progress-M of the same generation could carry.^[2] This propellant can be transferred to the Space Station's own propulsion system through fluid connectors in the docking ring, or it can alternatively be used by the Progress' thrusters to boost the station altitude or to change its orientation, or attitude, in space. In addition to propellant, the spacecraft can also carry up to 1,800 kilograms (4,000 lb) (6 cubic meters volume) of supplies in its forward pressurized cargo module (including a maximum of 40 kilograms (88 lb) of compressed air), but the combination of pressurized cargo and refuelling propellant cannot exceed 2,500 kilograms (5,500 lb) or the maximum capability of the launch vehicle. The tare weight of Progress-M1 is 5,050 kilograms (11,130 lb).^[3] Its KTDU-80 engine has a thrust of 2,950 newtons (660 lb_f) and uses up to 892 kilograms (1,967 lb) of propellant carried in four integrated spherical tanks for maneuvers such as docking and deorbiting the craft; 185 kilograms (408 lb) to 250 kilograms (550 lb) is typically left unused and hence available for the space station.

The Progress-M1 11F615A70 is a modernised variant of the earlier 11F615A55, with digital flight control systems replacing the earlier analogue ones. The older 11F615A55 spacecraft is no longer in use. It made eleven flights, the last of which, Progress M1-11, was deorbited in June 2004. The 11F615A70 was scheduled to make its first flight, Progress M1-01M, in 2011 but was cancelled.

Of the eleven 11F615A55 spacecraft launched, three flew to Mir, with the remainder being used to resupply the International Space Station.^[4] Ten of the spacecraft were used for traditional resupply missions, whilst the eleventh, Progress M1-5, was used instead to deorbit the Mir space station.^[5]

Progress-M1 spacecraft are launched by Soyuz rockets. Eight of the 11F615A55 spacecraft were launched by the Soyuz-U variant, whilst the remaining three; the sixth, seventh and ninth spacecraft, flew on the Soyuz-FG.^[6] 11F615A70 launches are expected to use the Soyuz-2 but was cancelled.

References

^ Krebs, Gunter. "Progress-M1 1 - 11 (11F615A55, 7KTGM1)". Gunter's Space Page. Retrieved 2009-08-04.
^ Krebs, Gunter. "Progress-M 1 - 13, 15 - 37, 39 - 67 (11F615A55, 7KTGM)". Gunter's Space Page. Retrieved 2009-08-04.
^ Jorgensen, Catherine A. (ed.). "International Space Station Evolution Data Book Volume I. Baseline Design Revision A (page 4.62)" (PDF). NASA/SP-2000-6109. Retrieved 2019-08-03.
^ Wade, Mark. "Progress M1". Encyclopedia Astronautica. Archived from the original on June 12, 2002. Retrieved 2009-08-04.
^ Zak, Anatoly (2001-01-24). "Mir "burial" mission launched". Spaceflight Now. Archived from the original on 2009-07-07. Retrieved 2009-08-04.
^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Archived from the original on 2009-11-13. Retrieved 2009-06-07.

Progress spacecraft

Versions

Missions

1970s	1978 Progress 1 2 3 4 1979 5 6 7
1980s	1980 Progress 8 9 10 11 1981 12 1982 13 14 15 16 1983 17 18 1984 19 20 21 22 23 1985 24 Kosmos 1669 1986 25 26 1987 27 28 29 30 31 32 33 1988 34 35 36 37 38 39 1989 40 41 M-1 M-2
1990s	1990 Progress M-3 42 M-4 M-5 1991 M-6 M-7 M-8 M-9 M-10 1992 M-11 M-12 M-13 M-14 M-15 1993 M-16 M-17 M-18 M-19 M-20 1994 M-21 M-22 M-23 M-24 M-25 1995 M-26 M-27 M-28 M-29 M-30 1996 M-31 M-32 M-33 1997 M-34 M-35 M-36 M-37 1998 M-38 M-39 M-40 1999 M-41 M-42
2000s	2000 Progress M1-1 M1-2 M1-3 M-43 M1-4 2001 M1-5 M-44 M1-6 M-45 M-SO1 M1-7 2002 M1-8 M-46 M1-9 2003 M-47 M1-10 M-48 2004 M1-11 M-49 M-50 M-51 2005 M-52 M-53 M-54 M-55 2006 M-56 M-57 M-58 2007 M-59 M-60 M-61 M-62 2008 M-63 M-64 M-65 M-01M 2009 M-66 M-02M M-67 M-03M M-MIM2
2010s	2010 Progress M-04M M-05M M-06M M-07M M-08M 2011 M-09M M-10M M-11M M-12M† M-13M 2012 M-14M M-15M M-16M M-17M 2013 M-18M M-19M M-20M M-21M 2014 M-22M M-23M M-24M M-25M 2015 M-26M M-27M† M-28M M-29M MS-01 2016 MS-02 MS-03 MS-04† 2017 MS-05 MS-06 MS-07 2018 MS-08 MS-09 MS-10 2019 MS-11 MS-12 MS-13
2020s	2020 Progress MS-14 MS-15 2021 MS-16 MS-17 MS-18 M-UM 2022 MS-19 MS-20 MS-21 2023 MS-22 MS-23 MS-24 MS-25 2024 MS-26 MS-27 MS-28 MS-29
Future	2025 MS-30 MS-31 MS-32 MS-33 2026 MS-34 MS-35 MS-36 MS-37

v t e Soyuz spacecraft variants
Early programme	Sever Soyuz 7K Soyuz 9K Soyuz 11K Soyuz-VI Soyuz P Soyuz PPK Soyuz R
7K series	Soyuz 7K-OK Soyuz 7K-L1 Soyuz 7K-LOK Soyuz 7K-TK Soyuz 7K-T/AF Soyuz 7K-OKS Soyuz 7K-T Soyuz 7K-TM Soyuz 7K-MF6
Later series	Soyuz T Soyuz TM Soyuz TMA Soyuz TMA-M Soyuz MS
Progress	Progress 7K-TG Progress M Progress M1 Progress MS
Other derivatives	Aelita Gamma

See also

References