
The Progress-M gained publicity in June 1997 when one crashed into the Spektr module, depressurizing it and severely damaging one of its solar panels. The Progress may have been overloaded with trash when the Mir crew, controlling it manually, were unable to get it to dock safely after a series of maneuvering and docking tests.
The Progress is similar to the Soyuz spacecraft but the Orbital module have been reconfigured to contain cargo.
The Cargo Module has a lenght of 3.0 m and a diameter of 2.3 m. Its habitable volume lies at 4.00 m3. It can take a payload of 1,340 Kg, and weighs with the payload a total of 2,520 kg.
The Descent module have been reconfigured to contain fuel for refueling Mir.
The Refuelling Module has a length of 2.2 m and a diameter of 2.2 m. It can have a payload of up to 975 Kg and the moulde weighs with the payload 1,846 kg.
The Service module is about the same on the Progress as on the Soyuz.
The Service module has a lenght of 2.3 m and a diameter of 2.2 m. It weighs 2,654 kg with the 500 Kg of fuel. The primary engine has a thrust of 417 kgf which gives 200 m/s of delta v.
| Module | Mass (Kg) | Length (m) | Max. Diameter (m) | Pressurized Volume (Cubic Meters) | No. of Solar Arrays/Area (Square Meters) | Power Output (KW) | Function |
|---|---|---|---|---|---|---|---|
| Progress M | 7,200 | 7 | 2.7 | 7.6 | 2/10 | 1.3 | Unmanned resupply & logistics |