|Given names:||Yuri Viktorovich||Aleksandr Ivanovich||Aleksandr Pavlovich|
|Position:||Commander||Flight Engineer||Flight Engineer|
|Spacecraft (Launch):||Soyuz TM-2||Soyuz TM-2||Soyuz TM-3|
|Launchtime:||21:38 UTC||21:38 UTC||01:59 UTC|
|Spacecraft (Landing):||Soyuz TM-3||Soyuz TM-2||Soyuz TM-3|
|Landingtime:||09:16 UTC||01:04 UTC||09:16 UTC|
|Mission duration:||326d 11h 37m||174d 03h 25m||160d 07h 16m|
|Given names:||Vladimir Georgiyevich||Aleksandr Aleksandrovich||Viktor Petrovich|
|Position:||Commander||Flight Engineer||Flight Engineer|
Launch from the Baikonur Cosmodrome; landing with Soyuz TM-3 spacecraft 140 km northeast of Arkalyk. It was the maiden manned voyage of a Soyuz TM spacecraft.
The MIR space station remained vacant after the departure of the Soyuz T-15 crew on July 16, 1986. In September 1986 the Altair/SR relay satellite Kosmos 1700 ceased operating and drifted off its geosynchronous orbit position. This reduced the station to communications via earth ground stations. The Progress 27 freighter docked with the station on January 18, 1986 and boosted MIR's mean altitude by 16 km to 345 km on January 26, 1986 in preparation for the launch of Soyuz TM-2. At this point only one of MIR's computers was functional.
Following a two day solo flight Soyuz TM-2 docked with the MIR-Progress 27 space station on February 07, 1987. The cosmonauts became the second resident crew.
This was first time of using the new docking system Kurs. Kurs was the successor to the IGLA system and today provides navigation beaconing for Russian space vehicles. When used for docking, the Soyuz or Progress vehicle broadcasts radar pulses from multiple antennas. The variation in strength between the antennas allows the system to compute relative position, attitude, and approach rate. The system is designed for automatic rendezvous and docking, but in an emergency cosmonauts may take command of the vehicle either locally, or from the MIR.
Following reactivation of the station and unloading of Progress 27, the freighter departed the station on February 23, 1987. It was followed by Progress 28 from March 05, 1987 - March 26, 1987, which then departed to clear the aft port for the large Kvant space station module.
Onboard the MIR the crew performed various scientific research work, including geophysical exploration of Middle Asia, the Kaspian Sea and the Caucasian region, spectralanalyses, production of semiconductor materials with the Korund 1M apparatus (48 different experiments) and photographs of the Earth surface. Other experiments were medical research, research work with fluids, building of metal alloys (copper and silver), plant growing experiments in the Phyton and Rost-apparatus, mounting the MKS-M2 optical spectrometer and a photometer for astrophysical experiments.
Early in the Soyuz TM-2 crew stay on MIR, the Kvant1 module was launched to automatically dock with MIR. Kvant consisted of the space station module (11 tons) and a unique FGB based vehicle called the Functional Service Module (FSM) (9.6 tons). The FSM carried out major maneuvers on April 02, 1987 and April 05, 1987. On April 5, 1987 its IGLA approach system began homing on MIR's aft port. The Tamyrs retreated to Soyuz TM-2 so that they could escape in the event the module got out of control. About 200 m out, the IGLA system lost its lock on MIRs aft port IGLA antenna. The cosmonauts watched from within Soyuz TM-2 as the Kvant / FSM combination passed within 10 m of the station.
Kvant and its FSM drifted 400 km from MIR before being guided back for a second docking attempt. The softdock occurred early on April 09, 1987. Kvants probe unit would not retract fully, preventing hard docking between MIR and Kvant. The Soviets left Kvant soft docked while they considered a solution. Maneuvers were impossible during this period, because the probe of the Kvant/FSM combination would wobble loosely in MIR's aft port drogue unit, banging the docking collars together.
The Kvant ('Quantum') 1 module was the first addition to the MIR core and contained a suite of scientific instruments for astrophysical observations and materials science experiments. The purpose of Kvant1 was to provide data and observations for research into the physics of active galaxies, quasars and neutron stars. The module also supported biotechnology experiments in the areas of anti-viral preparations and fractions. It was about 5.8 m long, had a maximum diameter of 4.15 m, and a mass of about 11 tons.
The module was divided into a pressurized laboratory compartment (40 cubic meters total pressurized volume) and a non-pressurized equipment compartment. The laboratory compartment was further divided into an instrumentation area and a living area, which were separated by an interior partition. A pressurized transfer chamber connected the core module with the laboratory chamber. The non-pressurized equipment contained power stabilizers.
The module was equipped with geodyne momentum wheels to replace the MIR core thruster system for routine attitude pointing. Attitude control thrusters were added to one of the external masts in 1992 to reduce fuel consumption of pointing maneuvers. One solar array wing from the Kristall module was transferred to Kvant1 in 1992. 2 new solar arrays (12 kW total) were delivered in 1995 to replace Kristall array. Initial docking maneuvers were performed by a service module which was jettisoned following docking. 2 Earth horizon sensors, 2 star sensors, and 3 star trackers are used for attitude knowledge.
The scientific payload consisted of:
TTM Coded Mask Imaging Spectrometer - a wide-angle camera that used a coded aperture mask to determine source location. It covered the energy range 2-30 keV with a 7.8 deg x 7.8 deg field of view. It could achieve an angular resolution of 2 arcminutes and a time resolution of 1 s.
HEXE (High Energy X-ray Experiment) - 4 detectors that covered the 15-200 keV energy range. The instrument had a 1.6 x1.6 deg field of view and had a maximum time resolution is 0.3-25 ms.
Sirene 2 Gas Scintillation Proportional Spectrometer - a gas scintillation proportional counter that covered the 2-100 keV energy range. It had a 3 x 3 deg field of view with a maximum time resolution of 1.25-2.5 ms.
Pulsar X-1 - 4 phoswich detectors that covered the 20-1300 keV energy range. It had a 3 x 3 deg field of view with a maximum time resolution of 10 s.
These experiments, taken together, are sometimes referred to as the Roentgen Observatory. All 4 experiments point toward the same source at the same time.
Glazar UV Spectrometer - covered wavelengths between 1150-1350 angstrom. The instrument could provide up to 1-2 angstrom resolution and has a 1.3 deg FOV.
Mariya magnetic spectrometer - measured high-energy electron and positron fluxes in near-Earth space.
Arfa-E - installed on the exterior of the module in January 1990 to investigate the Earth's ionosphere and magnetosphere by injecting electron beams perpendicular to the geomagnetic field.
On April 12, 1987 Yuri Romanenko and Aleksandr Laveykin exited MIR for the first EVA (3h 40m) to examine and, if possible, repair the problem with Kvant. They discovered a foreign object lodged in the docking unit, probably a trash bag they had left between Progress 28 and MIR's drogue. On command from the TsUP, Kvant extended its probe unit, permitting the cosmonauts to pull the object free and discard it into space. Kvant then successfully completed docking at a command from the ground. The Kvant FSM undocked from Kvant, freeing the module's aft port to fill in for the MIR aft port.
The crew entered Kvant on the next day and began unloading equipment into the base block. Kvant added 40 m³ of pressurized volume to MIR, bringing the total to about 130 m³. On April 16, 1987 the pointing motors on MIR's two solar arrays were linked to sensors on Kvant. Kvant carried stowed solar arrays intended to be attached to a fixture on top of the small-diameter section of the base block.
Progress 29 arrived and remained docked to the aft docking port of Kvant from April 23, 1987 - May 11, 1987. Beginning April 30, 1987, the crew tested orienting the MIR complex using Kvant's gyrodynes. In part this was in preparation for pointing the new module's roughly 1000 kg of astrophysical instruments. During this period, propellant was pumped through Kvant to MIR's ODU for the first time. The Elektron system aboard Kvant, which produced oxygen by electrolysis of water, was readied on May 08, 1987.
The USSR acknowledged that MIR was short on electricity. The situation became particularly difficult when melts lasting days were conducted using Korund 1-M. The MIR-2 crew spent most of May 1987 conducting medical experiments and Earth resources photography, activities which required little electricity.
Progress 30 arrived and remained docked to Kvant's aft port from May 21, 1987 - July 19, 1987.
The second EVA occurred on June 12, 1987 (1h 53m). Yuri Romanenko and Aleksandr Laveykin exited MIR's multiport node for the first of two EVAs to install the solar array delivered by Kvant. There was insufficient room available in the multiport node for two space-suited cosmonauts plus the main boom and first two sections of the new array, so Aleksandr Laveykin and Yuri Romanenko sealed the hatch between the Soyuz TM-2 docking module and orbital module and left the hatch between the orbital module and the multiport node open, creating an extended airlock. One cosmonaut worked outside while the other handed out needed parts. The main boom of the array was an extendible girder like the one assembled outside Salyut 7 by the MIR Expedition 1 / Salyut 7 Expedition 6 crew (Leonid Kizim and Vladimir Soloviyov, 1986).
In the third EVA on June 16, 1987 (3h 15m) the cosmonauts installed the remainder of the solar array, attached its electrical connections to the MIR power system, and extended it to its full 10.6-m length. The new, 22-24 m³ array brought MIR's total capacity to 11.4 kW.
The Roentgen Observatory on Kvant was uniquely placed to study Supernova 1987a in the Large Magellanic Cloud. The cosmonauts examined the exploding star during 115 sessions between June and September 1987.
Aleksandr Laveykin developed heart irregularities which made necessary his early return to Earth.
Soyuz TM-3 arrived at the station and docked to the aft Kvant port. It would remained docked to the station from July 22, 1987 - December 29, 1987. The visiting crew observed Syria and conducted materials processing experiments. Syrian guest cosmonaut Muhammed Faris and Soviet cosmonaut Aleksandr Viktorenko returned to Earth in Soyuz TM-2 with Aleksandr Laveykin. He was replaced by Aleksandr Aleksandrov, who had arrived aboard Soyuz TM-3. Yuri Romanenko and cosmonaut Aleksandr Aleksandrov performed more than 1000 astrophysical, geophysical, medical, biological and technological experiments.
The Soyuz spacecraft is composed of three elements attached end-to-end - the Orbital Module, the Descent Module and the Instrumentation/Propulsion Module. The crew occupied the central element, the Descent Module. The other two modules are jettisoned prior to re-entry. They burn up in the atmosphere, so only the Descent Module returned to Earth.
Having shed two-thirds of its mass, the Soyuz reached Entry Interface - a point 400,000 feet (121.9 kilometers) above the Earth, where friction due to the thickening atmosphere began to heat its outer surfaces. With only 23 minutes left before it lands on the grassy plains of central Asia, attention in the module turned to slowing its rate of descent.
Eight minutes later, the spacecraft was streaking through the sky at a rate of 755 feet (230 meters) per second. Before it touched down, its speed slowed to only 5 feet (1.5 meter) per second, and it lands at an even lower speed than that. Several onboard features ensure that the vehicle and crew land safely and in relative comfort.
Four parachutes, deployed 15 minutes before landing, dramatically slowed the vehicle's rate of descent. Two pilot parachutes were the first to be released, and a drogue chute attached to the second one followed immediately after. The drogue, measuring 24 square meters (258 square feet) in area, slowed the rate of descent from 755 feet (230 meters) per second to 262 feet (80 meters) per second.
The main parachute was the last to emerge. It is the largest chute, with a surface area of 10,764 square feet (1,000 square meters). Its harnesses shifted the vehicle's attitude to a 30-degree angle relative to the ground, dissipating heat, and then shifted it again to a straight vertical descent prior to landing.
The main chute slowed the Soyuz to a descent rate of only 24 feet (7.3 meters) per second, which is still too fast for a comfortable landing. One second before touchdown, two sets of three small engines on the bottom of the vehicle fired, slowing the vehicle to soften the landing.
A new long duration record was set by Yuri Romanenko (326 days).
Last update on August 14, 2015.