Information about Soyuz Fg
The launch of Soyuz TMA-9 atop a Soyuz-FG rocket. The launch of Soyuz TMA-9 atop a Soyuz-FG rocket. | |
| Fact sheet | |
|---|---|
| Function | Orbital carrier rocket |
| Manufacturer | TsSKB-Progress |
| Country of origin | Russia |
| Size | |
| Height | 49.5 m for Soyuz-FG and 42.5 m for Soyuz-FG/Fregat |
| Diameter | 10.3 m |
| Mass | 305,000 kg (672,000 lb) |
| Stages | 2 (Soyuz FG) or 3 (Soyuz-FG/Fregat) |
| Capacity | |
| Payload to LEO | 7,100 kg for Soyuz-FG and 7,800 kg for Soyuz-FG/Fregat |
| Payload to 800km SSO (only for Soyuz-FG/Fregat) | 4,500 kg (9,900 lb) |
| Launch History | |
| Status | Active |
| Launch sites | LC-1 (Soyuz-FG) & LC-31 (Soyuz-FG/Fregat), Baikonur |
| Total launches | 20 (FG: 14, FG/Fregat: 6) |
| Successes | 20 |
| Maiden flight | Soyuz-FG: 20 May 2001 Soyuz-FG/Fregat 2 June 2003 |
| Boosters (Stage 0) | |
| '''No boosters | 4 |
| Engines | 1 RD-117 |
| Thrust | 1,021.097 kN |
| Specific impulse | 310 sec |
| Burn time | 120 seconds |
| Fuel | LOX/RP-1 |
| First Stage | |
| Engines | 1 RD-118 |
| Thrust | 999.601 kN (224,719 LBf) |
| Specific impulse | 311 sec |
| Burn time | 286 seconds |
| Fuel | LOX/RP-1 |
| Second Stage | |
| Engines | 1 RD-0124 |
| Thrust | 294 kN (66,093 LBf) |
| Specific impulse | 359 sec |
| Burn time | 300 seconds |
| Fuel | LOX/RP-1 |
| Third Stage (Optional) - Fregat | |
| Engines | 1 S5.92 |
| Thrust | 19.6 kN (4,406 LBf) |
| Specific impulse | 327 sec |
| Burn time | 877 seconds |
| Fuel | N2O4/UDMH |
Since 30 October, 2002 it has been used by Russian Federal Space Agency only for bringing Soyuz-TMA manned spacecraft to the ISS. As of April, 2007 Soyuz-FG has performed 14 flights, bringing to the ISS 3 Progress-M1 and 11 Soyuz-TMA spacecraft, with its last launch on 10 October, 2007. All launches have been successful.
Another version of the Soyuz-FG is the Soyuz-FG/Fregat with Fregat as its 3rd stage, developed and produced by Lavochkin Association in Khimki. A European-Russian company Starsem ownes all rights to launches using this version. As of May, 2007 there have been 6 launches of Soyuz-FG/Fregat with commercial payloads. Its maiden flight occurred on 2 June, 2003.
The analog control system of this spacecraft significantly limits its capabilities however and it will eventually be replaced by the Soyuz-2 LV.
The Soyuz-FG is launched from the Baikonur Cosmodrome, Launch site LC-1 for Soyuz-FG and LC-31 for Soyuz-FG/Fregat.
Launch history
| Date and Time (GMT) | Configu- ration |
Serial Number | Launch Site | Result | Payload | Remarks |
|---|---|---|---|---|---|---|
| 20 May 2001 22:32 | Soyuz-FG | F15000-001 | LC-1, Baikonur | Success | Progress-M1 6 | ISS Logistics |
| 26 November 2001 18:24 | Soyuz-FG | F15000-002 | LC-1, Baikonur | Success | Progress-M1 7 | ISS Logistics |
| Kolibri 2000 | ||||||
| 25 September 2002 16:58 | Soyuz-FG | E15000-003 | LC-1, Baikonur | Success | Progress M1-9 | ISS Logistics |
| 30 October 2002 16:58 | Soyuz-FG | E15000-004 | LC-1, Baikonur | Success | Soyuz TMA-1 | Manned flight with 3 Cosmonauts ISS escape craft |
| 26 April 2003 03:53 | Soyuz-FG | 15000-006 | LC-1, Baikonur | Success | Soyuz TMA-2 | Manned flight with 2 Cosmonauts ISS Expedition 7 |
| 2 June 2003 18:24 | Soyuz-FG/Fregat | E15000-005/ ST-11 | LC-31, Baikonur | Success | Mars Express | Mars orbiter |
| Beagle 2 | Mars lander Launched successfully but later failed | |||||
| 18 October 2003 05:38 | Soyuz-FG | D15000-007 | LC-1, Baikonur | Success | Soyuz TMA-3 | Manned flight with 3 Cosmonauts ISS Expedition 8 |
| 27 December 2003 21:30 | Soyuz-FG/Fregat | D15000-008/ ST-12 | LC-31, Baikonur | Success | Amos-2 | Communi- cations satellite |
| 19 April 2004 05:19 | Soyuz-FG | D15000-009 | LC-1, Baikonur | Success | Soyuz TMA-4 | Manned flight with 3 Cosmonauts ISS Expedition 9 |
| 14 October 2004 03:06 | Soyuz-FG | Zh15000-012 | LC-1, Baikonur | Success | Soyuz TMA-5 | Manned flight with 3 Cosmonauts ISS Expedition 10 |
| 15 April 2005 00:46 | Soyuz-FG | Zh15000-014 | LC-1, Baikonur | Success | Soyuz TMA-6 | Manned flight with 3 Cosmonauts ISS Expedition 11 |
| 13 August 2005 23:28 | Soyuz-FG/Fregat | Zh15000-011/ ST-13 | LC-31, Baikonur | Success | Galaxy 14 | Communi- cations satellite |
| 1 October 2005 03:54 | Soyuz-FG | Zh15000-017 | LC-1, Baikonur | Success | Soyuz TMA-7 | Manned flight with 3 Cosmonauts ISS Expedition 12 |
| 9 November 2005 03:33 | Soyuz-FG/Fregat | Zh15000-010/ ST-14 | LC-31, Baikonur | Success | Venus Express | Venus orbiter |
| 28 December 2005 05:19 | Soyuz-FG/Fregat | Zh15000-016/ ST-15 | LC-31, Baikonur | Success | GIOVE-A | Navigation satellite |
| 30 March 2006 02:30 | Soyuz-FG | P15000-018 | LC-1, Baikonur | Success | Soyuz TMA-8 | Manned flight with 3 Cosmonauts ISS Expedition 13 |
| 18 September 2006 04:08 | Soyuz-FG | ?15000-023 | LC-1, Baikonur | Success | Soyuz TMA-9 | Manned flight with 3 Cosmonauts ISS Expedition 14 |
| 7 April 2007 17:31 | Soyuz-FG | LC-1, Baikonur | Success | Soyuz TMA-10 | Manned flight with 3 Cosmonauts ISS Expedition 15 | |
| 29 May 2007 20:31 | Soyuz-FG/Fregat | LC-31, Baikonur | Success | Globalstar | Comsat | |
| Globalstar | Comsat | |||||
| Globalstar | Comsat | |||||
| Globalstar | Comsat | |||||
| 10 October 2007 13:22 [1] | Soyuz-FG | LC-1, Baikonur | Success | Soyuz TMA-11 | Manned flight with 3 Cosmonauts ISS Expedition 16 | |
| 20 October 2007 20:12 | Soyuz-FG/Fregat | LC-31, Baikonur | In progress | Globalstar | Comsat | |
| Globalstar | Comsat | |||||
| Globalstar | Comsat | |||||
| Globalstar | Comsat |
See also
- R-7
- Soyuz launch vehicle
- Soyuz spacecraft
- Soyuz programme
- Soyuz-U
- International Space Station
- Russian Federal Space Agency
- Starsem
External links
- Russian Federal Space Agency about Soyuz-FG
- Russian Federal Space Agency about Soyuz-FG/Fregat (in English)
- LV's manufacturer TsSKB-Progress about Soyuz-FG(in Russian)
List of expendable launch vehicles | |
|---|---|
| Current: | |
| Planned: | |
| Historical: | |
Globalstar is a low Earth orbit (LEO) satellite constellation for telephone and low-speed data communications, similar to (and competing with) the Iridium satellite system.
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Baikonur Cosmodrome (Kazakh: Байқоңыр ғарыш айлағы, Bayqoñır ğarış aylağı; Russian:
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Soyuz TMA-9
Mission insignia
Mission statistics
Mission name: Soyuz TMA-9
Spacecraft name: Soyuz TMA
Call sign: Vostok
Number of crew members: 3
Launch pad: Gagarin's Start
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Mission insignia
Mission statistics
Mission name: Soyuz TMA-9
Spacecraft name: Soyuz TMA
Call sign: Vostok
Number of crew members: 3
Launch pad: Gagarin's Start
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launch vehicle or carrier rocket is a rocket used to carry a payload from the Earth's surface into outer space. A launch system includes the launch vehicle, the launch pad and other infrastructure.
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Anthem
Hymn of the Russian Federation
Capital
(and largest city) Moscow
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Hymn of the Russian Federation
Capital
(and largest city) Moscow
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1 metre =
SI units
1000 mm 0 cm
US customary / Imperial units
0 ft 0 in
The metre or meter[1](symbol: m) is the fundamental unit of length in the International System of Units (SI).SI units
1000 mm 0 cm
US customary / Imperial units
0 ft 0 in
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1 metre =
SI units
1000 mm 0 cm
US customary / Imperial units
0 ft 0 in
The metre or meter[1](symbol: m) is the fundamental unit of length in the International System of Units (SI).SI units
1000 mm 0 cm
US customary / Imperial units
0 ft 0 in
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1 metre =
SI units
1000 mm 0 cm
US customary / Imperial units
0 ft 0 in
The metre or meter[1](symbol: m) is the fundamental unit of length in the International System of Units (SI).SI units
1000 mm 0 cm
US customary / Imperial units
0 ft 0 in
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kilogram or kilogramme (symbol: kg) is the SI base unit of mass. The kilogram is defined as being equal to the mass of the International Prototype Kilogram (IPK), which is almost exactly equal to the mass of one liter of water.
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pound or pound-mass (abbreviations: lb, ℔, lbm, or sometimes in the United States: #) is a unit of mass (sometimes called 'weight' in everyday parlance) in a number of different systems, including English units, Imperial units, and United
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Payload may refer to:
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- Cargo, goods or produce being delivered or transported
- Payload (air and space craft), the net carrying capacity of an aircraft or spacecraft (as distinct from throw weight)
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Low Earth Orbit (LEO) is generally defined as an orbit within the locus extending from the Earth’s surface up to an altitude of 2,000 km. Given the rapid orbital decay of objects below approximately 200 km, the commonly accepted definition for LEO is between 200 - 2000 km
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kilogram or kilogramme (symbol: kg) is the SI base unit of mass. The kilogram is defined as being equal to the mass of the International Prototype Kilogram (IPK), which is almost exactly equal to the mass of one liter of water.
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kilogram or kilogramme (symbol: kg) is the SI base unit of mass. The kilogram is defined as being equal to the mass of the International Prototype Kilogram (IPK), which is almost exactly equal to the mass of one liter of water.
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sun-synchronous orbit (sometimes incorrectly called a heliosynchronous orbit) is a geocentric orbit which combines altitude and inclination in such a way that an object on that orbit passes over any given point of the Earth's surface at the same local solar time.
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kilogram or kilogramme (symbol: kg) is the SI base unit of mass. The kilogram is defined as being equal to the mass of the International Prototype Kilogram (IPK), which is almost exactly equal to the mass of one liter of water.
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pound or pound-mass (abbreviations: lb, ℔, lbm, or sometimes in the United States: #) is a unit of mass (sometimes called 'weight' in everyday parlance) in a number of different systems, including English units, Imperial units, and United
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Gagarin's Start
Soyuz TMA-3 is launched from Gagarin's Start
Launch Site Baikonur Cosmodrome
Location 45.920278°N
63.342222°E
Short name
Operator Soviet space program, Russian Space Agency
Total launches
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Soyuz TMA-3 is launched from Gagarin's Start
Launch Site Baikonur Cosmodrome
Location 45.920278°N
63.342222°E
Short name
Operator Soviet space program, Russian Space Agency
Total launches
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Baikonur Cosmodrome (Kazakh: Байқоңыр ғарыш айлағы, Bayqoñır ğarış aylağı; Russian:
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May 20 is the 1st day of the year (2nd in leap years) in the Gregorian calendar. There are 0 days remaining.
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The newton (symbol: N) is the SI derived unit of force, named after Sir Isaac Newton in recognition of his work on classical mechanics.
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Definition
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Specific impulse (usually abbreviated Isp) is a way to describe the efficiency of rocket and jet engines. It represents the impulse (change in momentum) per unit of propellant.
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Lox is salmon fillet that has been cured. In its most popular form, it is thinly sliced (less than 5 millimeters in thickness) and, typically, served on a bagel, often with cream cheese.
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RP-1 (alternately, Rocket Propellant-1 or Refined Petroleum-1) is a highly refined form of kerosene outwardly similar to jet fuel, used in the United States as a rocket fuel.
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Thrust is a reaction force described quantitatively by Newton's Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.
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The newton (symbol: N) is the SI derived unit of force, named after Sir Isaac Newton in recognition of his work on classical mechanics.
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Definition
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