Cargo spacecraft "Progress M-50"

CIS



Launch, orbit & landing data:

Designation 28399 / 04032A
Launch date - time 11 Aug 2004 - 05:03:07 UT
Launch site Baikonur, LC1
Launch vehicle  Soyuz 11A511U (s/n°: D15000-685)
OKB name - S/N° 7K-TGM (n°350)
Mass (kg) 7283
Total cargo mass (kg) 
Earth orbit on :
   - Perigee / Apogee 193 x 251 km
   - Inclination 51.7°
   - Period 88.7 min


Docking date - time 14 Aug 2004 - 05:01:08 UT
Target spacecraft/port ISS/Zvezda SM (rear port)
Orbital parameters on 14 Aug:
   - Perigee / Apogee 353 / 360 km
   - Inclination 51,63°
   - Period 91,67 min
Undocking date - time 22 Dec 2004 - 19:38 UT
Deorbit burn date - time 22 Dec 2004 - 22:32:06 UT
over the Pacific
Destroyed date - time 22 Dec 2004 - 23:23:38 UT
Flight Duration (dd:hh:min) 
Nbr orbits 

Mission:

Delivery of cargo and propellant to the International Space Station, the 15th cargo ship to ISS. (mission ISS-15P)

05 Aug 2004 - Preparation of Progress M-50 on Baikonur Cosmodrome:

Designers inspection of the Progress M-50 cargo vehicle was completed in the spacecraft processing facility.

640x480 (103 Kb) 640x480 (98 Kb) 640x480 (115 Kb)

Payload shroud roll on to the Progress M-50 spacecraft was completed.

640x480 (89 Kb)640x480 (110 Kb)640x480 (102 Kb)

640x480 (99 Kb)640x480 (91 Kb)640x480 (87 Kb)


All photos by RSC Energia.


Mission report:

At 9 hours 3 minutes 7 seconds Moscow Time the Rocket and Space Complex Soyuz-U/Progress M-50 was launched.
The objective of the launch performed under the International Space Station (ISS) Mission Program and the commitments undertaken by the Russian side is to deliver to the station the cargoes required to keep its operation, maintain crew living conditions and activities, refuel its tanks with propellant and gases, ensure orbital correction.
The mission of the cargo transport vehicle has designation 15P under the ISS deployment program.
The cargo space vehicle compartment of refueling propellants accommodates 442 kg of fuel, 28 kg of oxygen, 21 kg of air, 420 kg of potable water. Its cargo bay contains some 1.4 tons of dry cargoes, involving food products, equipment and facilities for the station onboard systems, medical equipment, underclothes, personal hygiene and individual protection aids, sets of onboard documentation, video-and photographic materials, parcels for crewmembers, structural members, payloads for the USOS, equipment and materials for conducting space experiments.
The cargo transport vehicle was put into orbit with maximum and minimum altitudes of 250,9 kg and 192.5 km, respectively; orbital period of 88,65 min and inclination of 51.65°.
Its onboard systems operate normally.
The cargo transport vehicle is to dock with the ISS on August 14th, 2004 approaching an axial docking assembly of the Russian Zvezda Service Module. The estimated time of coming in contact with the docking assembly is 09 : 02. The docking assembly was released on July 30th, 2004, when the Progress M-49 cargo transport vehicle operating as part of the Complex since May 27th, 2004, had departed from the station.
After undocking with the ISS, that space vehicle was moved away at a safe distance and subsequently transferred to the trajectory of descent and escaping the orbit and, finally, to the preset area in the Pacific Ocean waters.
The decision on the Soyuz-U/Progress M-50 Complex launch was taken by the State Commission (with N.F. Moiseev, V.A. Grin as its Co-Chairmen) relying on the Technical Management's conclusion on the readiness of the Complex and the ground infrastructure components involved in the ISS Program implementation.
The Complex prelaunch processing was carried out under direct lead of the Technical Management (Yu.P. Semenov, Technical Manager of the Russian manned space programs, General Designer of RSC Energia after S.P. Korolev, the RAS academician).
The flight of the cargo transport vehicle and the ISS Russian Segment is commanded by the Lead Operational Control Team (LOCT) based in Moscow Mission Control Center (MCC-M, Korolev). The Flight Director is Pilot-Cosmonaut V.A. Solovyov from RSC Energia after S.P. Korolev. The Orbital Complex is flying in a near-earth orbit with the following parameters: maximum and minimum altitudes of 378.2 km and 355.0 km, respectively; an orbital period of 91.6 min and inclination of 51.65°. The ISS Russian Segment incorporates Functional Cargo Block Zarya, Zvezda Service Module, docking module Pirs and Soyuz TMA-4 manned transport spacecraft. The USOS is operating made up of the following components: Unity module, Destiny module, airlock Quest and multielement truss structure with solar arrays deployed. Total mass of the Complex is about 176.4 tons.
By telemetry data and reports produced by the crewmembers of Expedition 9, Russian cosmonaut Gennady Padalka (Commander) and American astronaut Michael Fincke (Flight Engineer), all onboard systems of the Orbital Complex are operating in design modes.

On 14 Aug., following a three-day free flight in near-earth orbit, the Russian Progress M-50 cargo vehicle docked to the International Space Station (ISS).
The vehicle approached a free axial docking port of the Russian Service Module Zvezda. At 9:01:08 Moscow time the vehicle came into contact with the station port. The vehicle rendezvous with the ISS, fly-about and docking were performed in the automatic mode. During the vehicle closing to the station, fly-about and final approach the vehicle and Space Station were within the Russian ground site coverage.
The Expedition crew ISS-9 consisting of Russian cosmonaut Gennady Padalka (Commander, Yu.A. Gagarin CTC RSRI) and American astronaut Michael Fincke (Flight Engineer, NASA) working onboard the station monitored the implementation of the approach and docking processes.
Progress M-50 delivered 2566 kg of various cargoes including 1405 kg of dry cargoes consisting of foodstuff, equipment and facilities for the station onboard systems, medical equipment, underwear, personal hygiene items and individual protection gear, flight-data files, video and photo materials, parcels for the crew, structural elements, payloads for the USOS, hardware and materials for space experiments.
The ISS-9 crew will have to unload the vehicle and accommodate the delivered cargoes on the Station, and load the wasted materials and equipment to the vehicle.
The on-orbit complex ISS of more than 183 tons performs a near-orbit flight with the following parameters: maximum altitude of 377.6 km, minimum altitude of 354.2 km, period of revolution of 91.6 min.


Ref.: #3(SD386), #7(JR541), #21, #87, #97, #210 - update: 19.05.05 Home