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Progress M1-5 is
carrying 2.5 times more fuel than normal for a resupply mission
instead of other cargoes like equipment, food and water. The
flight will take twice as long as a conventional cargo mission to
Mir. The longer trip is designed to conserve the cargo
spacecraft's propellant for the deorbiting procedure, which will
require a lot of fuel. Instead of using its fuel-thirsty main
engine, the Progress M1-5 will use its smaller engines for
approach and orientation. The spacecraft will dock to Mir’s
Kvant module. The extra propellant will be used to assist in the
deorbiting of the Mir space station in early March. The Progress
propulsion system and fuel will be used to lower the station out
of its orbit to about 80 km (42 nmi) to make a reentry into the
Earth’s atmosphere.
On March 4 and 5,
the Progress is planned to fire three pulses to brake the station.
The first two pulses will decrease Mir’s speed by 7 meters per
second each, while the third one will decrease the station’s
speed by 14 meters per second. On March 6, the Progress will
generate the final pulse which should decrease Mir’s speed by
17.3 meters per second and cause it to plunge into the Pacific
Ocean later that day. Remains of the station are expected to fall
in the Pacific Ocean, east of New Zealand.
| Progress
M1-5
|
|
SPACECRAFT
|
| Int'l Designation |
2001
003A
|
Launched
|
| Owner / Sponsor |
Rosaviakosmos
|
| Mission |
Cargo
|
| Launch Mass |
|
| Mission Orbit |
LEO
|
51.6°
|
| Design Life |
|
| Power (EOL) |
|
|
LAUNCH
|
| Launch Vehicle
Model |
Soyuz
U |
| Launch Date / Time |
2001
Jan 24
|
22:09
|
|
Financial
|
| Satellite cost |
|
| Web Links |
|
|