Chronology - Quarter 1 2001 home
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2001 January 3 -
  • Advent completes construction of full-scale propulsion system. Nation: USA. Program: X-Prize. Advent Launch Systems (Houston, Texas, USA) completes construction of full-scale propulsion system.
2001 January 6 -
  • Yuan Wang deployed for Shenzhou 2 flight Nation: China. Spacecraft: Shenzhou. China reported that the four Yuan Wang tracking ships celebrated the New Year on remote oceans. Yuan Wang 1 and 2 were in the Pacific Ocean, Yuan Wang 4 had arrived in the Indian Ocean, and Yuan Wang 3 was en route to the Atlantic Ocean. References: 424.
2001 January 9 - 17:00 GMT - Launch Site: Jiuquan. Launch Complex: SLS. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-2F. LV Configuration: Chang Zheng 2F CZ2F-2 (65).
  • Shenzhou 2 Nation: China. Mass: 7,400 kg (16,300 lb). Class: Manned. Type: Spacecraft. Spacecraft: Shenzhou. Manufacturer: China Academy of Launch Vehicle Technology. Agency: CASC. Perigee: 330 km (200 mi). Apogee: 346 km (214 mi). Inclination: 42.60 deg. COSPAR: 2001-001A. USAF Sat Cat: 26664. Duration: 6.77 days. Decay Date: 2001-01-16. The second unmanned test flight of the Shenzhou manned spacecraft design carried a monkey, a dog and a rabbit in a test of the spaceship's life support systems. Shenzhou 2 was the first test of an all-up flight model of the spacecraft, with a functioning orbital module. It was also the most ambitious space science laboratory ever launched by China. It carried 64 scientific payloads: 15 in the re-entry module, 12 in the orbital module and 37 on the forward external pallet. These included a micro-gravity crystal growing device; life sciences experiments with 19 species of animals and plants, cosmic ray and particle detectors; and China's first gamma ray burst detectors.

    The launch was originally scheduled for January 5, but the second stage of the launch vehicle was dented by an access platform while being prepared for roll-out in the vehicle assembly building. This caused several days of delay until it was cleared for flight. Shenzhou 2 made three orbit-raising manoeuvres during its flight, reaching a 330 x 345 km orbit by the end of the initial phase of the mission. Ninety minutes before landing the orbital module depressurised, and the spacecraft went briefly out of control. However this was regained after venting of the atmosphere from the module ended. The descent module and service modules separated from the forward orbital module and external pallet normally. After retrofire by the service module, it separated and the descent module landed at 11:22 GMT on January 16 in Inner Mongolia. Lack of post-recovery photographs led to speculation that the recovery may not have been completely successful. The Shenzhou orbital module had its own solar panels and remained operational in orbit, conducting scientific experiments. It was actively controlled for six months, maneuvering in orbit several times (reaching a final orbit of 394 x 405 km). It then was allowed to decay and reentered the atmosphere at 09:05 GMT on August 24, 2001. The reentry point was near 33.1 deg S in latitude and 260.4 deg E in longitude, over the western Pacific Ocean between Easter Island and Chile. References: 2, 296, 460, 552, 554.

2001 January 10 - 22:09 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 44P. LV Configuration: Ariane 44P-3 V137.
  • Turksat 2A Nation: Turkey. Payload: Eurasiasat 1. Mass: 3,535 kg (7,793 lb). Class: Communications. Spacecraft: Spacebus 3000. Manufacturer: Alcatel Space. Agency: Eurasisa. Perigee: 35,764 km (22,222 mi). Apogee: 35,808 km (22,250 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2001-002A. USAF Sat Cat: 26666. Communications satellite. Launch delayed from December 8, 2000 and January 8. The Turksat 2A (Eurasiasat 1) satellite was an Alcatel Spacebus 3000B3 with a dry mass of 1577 kg (launch mass 3535 kg) and a 37m solar panel span. The satellite was placed in a 162 x 36742 km x 2.9 deg orbit; by January 13 the perigee had been raised to 21185 km. The satellite had 36 Ku-band transponders and three antennae. The dual name was probably due to the dual ownership of the spacecraft: 75% by Turk Telecom and 25% by the manufacturer Alcatel Space Company. The 3.4 tonne, 9 kW spacecraft was to provide direct-to-home voice, video, and data transmissions to countries between central Europe and the Indian subcontinent, through its 32 "BSS- and FSS-bands" transponders, after parking over 42 deg-E longitude (replacing the aging Turksat 1C). Positioned in geosynchronous orbit at 42 deg E in 2001 As of 4 September 2001 located at 41.96 deg E drifting at 0.016 deg E per day. As of 2007 Mar 11 located at 42.03E drifting at 0.008E degrees per day. References: 2, 296, 552, 554.
2001 January 11 -
  • The release of the Congressionally-chartered Space Commission report set the stage for significant organizational and mission changes for Air Force Space Command. Nation: USA. References: 569.
2001 January 15 -
  • Stardust, Earth Flyby Nation: USA. Spacecraft: Stardust.
2001 January 17 - 04:31 GMT - Launch Site: Balasore. Launch Complex: IC4. Launch Pad: -. Launch Vehicle: Agni. Model: Agni 2.
  • Agni RV Mk 2 Research and development launch Nation: India. Agency: IDRDL. Apogee: 1,000 km (600 mi). References: 2.
2001 January 24 - 04:28 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. LV Configuration: Soyuz 11A511U K15000-673.
  • Progress M1-5 Nation: Russia. Program: Mir. Payload: Progress M1 s/n 254. Mass: 7,300 kg (16,000 lb). Class: Manned. Type: Logistics. Spacecraft: Progress M1. Manufacturer: RKK Energiya. Agency: RAKA. Perigee: 278 km (172 mi). Apogee: 299 km (185 mi). Inclination: 51.60 deg. COSPAR: 2001-003A. USAF Sat Cat: 26688. Duration: 58.00 days. Decay Date: 2001-03-23. Mir Deorbiting mission. Launch delayed from January 16 and 18. The Mir station had a power failure on January 18, delaying the launch of the Progress cargo ship that was to deorbit it for a few days. Nick-named "Hearse", it was to deliver the 130 tonne Mir station to its cremation over the southern Pacific. Six cosmonauts were on "Hot-Standby" to reach Mir in the event the automatic docking failed. Progress M1-5 carried 2677 kg of fuel. A special three-day fuel-economy approach was be used to keep as much fuel as possibile for the deorbit. Progress M1-5 docked with the +X Kvant port at 0533 GMT on January 27. It later undocked and was deorbited over the Pacific together with Mir on 23 March. References: 2, 296, 552, 554.
2001 January 26 - 03:57 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aries. LV Configuration: Aries NTW Aegis Target.
  • TTV-2 (FTR-1A) Target mission Nation: USA. Agency: USN. Apogee: 300 km (180 mi). References: 2.
2001 January 26 - 04:03 GMT - Launch Site: Barking Sands. Launch Complex: POA. Launch Pad: -. Launch Vehicle: Standard-ER. Model: Standard SM-3. LV Configuration: SM-3 Aegis FTR-1A.
  • Test mission Nation: USA. Agency: USN. Apogee: 100 km (60 mi). References: 2.
2001 January 30 - 07:55 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: SLC17A. Launch Vehicle: Delta. Model: Delta 7925-9.5. LV Configuration: Delta 7925-9.5 D283.
  • USA 156 Nation: USA. Program: Navstar. Payload: GPS 2R-7 / GPS SVN 54. Mass: 2,032 kg (4,479 lb). Class: Navigation. Spacecraft: GPS Block 2R. Manufacturer: Lockheed Martin Space Systems. Agency: USAF. Perigee: 20,157 km (12,524 mi). Apogee: 20,208 km (12,556 mi). Inclination: 55.20 deg. Period: 718.00 min. COSPAR: 2001-004A. USAF Sat Cat: 26690. GPS Block IIR production no. SV 14. Placed in Plane E Slot 4 of the constellation. References: 2, 296, 552, 554.
2001 February 7 - 09:28 GMT - Launch Site: Vandenberg. Launch Complex: LF10. Launch Pad: -. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT175GB.
  • GT175GB Functional Dependency gate operational test launch Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi). References: 2.
2001 February 7 - 23:05 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 44L. LV Configuration: Ariane 44L-3 V139.
  • Sicral Nation: Italy. Payload: Sicral 1. Mass: 2,596 kg (5,723 lb). Class: Communications. Spacecraft: Italsat. Manufacturer: SITAB Consortium (Alenia Aerospazio). Agency: ADI. Perigee: 35,773 km (22,228 mi). Apogee: 35,801 km (22,245 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2001-005A. USAF Sat Cat: 26694. Sicral, (Sistema Italiana de Communicazione Riservente Allarmi) was a communications satellite for the Italian defense ministry's procurement division, the Segretariato Generale della Difesa's Direzione Nazionale degli Armamenti. Sicral was built by Alenia Aerospazio and derived from the Italsat series. Its mass was 2596 kg full, 1253 kg dry and it carried a liquid apogee engine. The 3.3 kW, 3.4 m x 4.9 m, triaxially-stabilized spacecraft carried a total of nine transponders in the SHF-, UHF-, and EHF-bands to enable secure communications after parking over 16.2 deg-E longitude. Positioned in geosynchronous orbit at 16 deg E in 2001 As of 26 August 2001 located at 16.27 deg E drifting at 0.004 deg W per day. As of 2007 Mar 9 located at 16.34E drifting at 0.018E degrees per day. References: 2, 296, 552, 554.
  • Skynet 4F Nation: UK. Program: Skynet. Mass: 2,596 kg (5,723 lb). Class: Communications. Type: Military. Spacecraft: ECS/OTS. Manufacturer: SITAB Consortium (Alenia Aerospazio). Agency: UK MoD. Perigee: 35,772 km (22,227 mi). Apogee: 35,801 km (22,245 mi). Inclination: 2.90 deg. Period: 1,436.10 min. COSPAR: 2001-005B. USAF Sat Cat: 26695. Skynet 4F was a communications satellite for the UK Ministry of Defense, and the last of the venerable ECS (European Communications Satellite) class of satellites built by Astrium/Stevenage. It carried a Thiokol Star 30 apogee motor and its mass was 1489 kg full, 830 kg dry - a dry mass more than twice the first OTS. The spacecraft carried a total of eight transponders in the SHF-, UHF-, and S-bands to provide secure communications after parking over either 1 deg-E or 6 deg-W. Positioned in geosynchronous orbit at 6 deg E in 2001 As of 5 September 2001 located at 8.77 deg E drifting at 0.284 deg W per day. As of 2007 Mar 10 located at 6.01E drifting at 0.004E degrees per day. References: 2, 296, 552, 554.
2001 February 7 - 23:13 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-98.
  • STS-98 Nation: USA. Program: ISS. Payload: Atlantis F23. Mass: 90,225 kg (198,912 lb). Class: Manned. Type: Spaceplane. Spacecraft: Atlantis. Manufacturer: Boeing. Agency: NASA JSC. Perigee: 183 km (113 mi). Apogee: 337 km (209 mi). Inclination: 51.30 deg. Period: 89.71 min. COSPAR: 2001-006A. USAF Sat Cat: 26698. Duration: 12.89 days. Decay Date: 2001-02-20. Crew: Cockrell, Polansky, Curbeam, Ivins, Jones. Flight: STS-98. ISS Assembly flight. Launch delayed from January 18 and February 6. International Space Station assembly mission; delivered the Destiny and PMA-2 modules. Destiny was an American ISS module, an 8.4 meter long and 4.2 meter wide cylindrical structure with a mass of 15 tonnes. It was to function as a science and technology module and the primary control module for the ISS. The shuttle orbiter was placed in an initial 74 x 323 km x 51.6 deg orbit. At 2357 GMT the OMS engines fired for the OMS-2 burn which raised Atlantis' orbit to 204 x 322 km x 51.6 deg. Atlantis docked with the Station at 1651 GMT on February 9 at the PMA-3 port on Unity's nadir. At 1500 GMT on Feb 10 Marsha Ivins used the RMS arm to unberth the PMA-2 docking port from Unity. Tom Jones and Bob Curbeam then conducted three spacewalks on Februay 10 to 14 to attach the Destiny and PMA-2 modules to the station. The crew also delivered over a tonne of food, fuel and equipment to the ISS. Atlantis undocked from Alpha at 1406 GMT on February 16. Atlantis landed at Edwards AFB on February 20; plans to land on February 18 and 19 were called off due to persistent wind problems at Kennedy Space Center. The deorbit burn was at 1927 GMT and lowered the orbit from 370 x 386 km to about 50 x 380 km. The nominal entry interface at 122 km came at 2002 GMT and touchdown on runway 22 was at 20:33 GMT. On March 1 Atlantis was flown on the back of NASA's SCA 911 carrier aircraft to Altus AFB, Oklahoma, en route to Kennedy. References: 2, 296, 552, 554.
2001 February 8 -
  • Discovery of the SAU 094 Meteorite (Mars Meteorite) Nation: Oman.
2001 February 9 - 04:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9CM1. LV Configuration: Black Brant 9CM1 NASA 36.198UG.
  • JHU FOT 16 Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi). References: 2.
2001 February 10 - 15:50 GMT -
  • EVA STS-98-1 Nation: USA. Program: ISS. Spacecraft: International Space Station. Crew: Jones, Curbeam. Flight: STS-98. EVA Duration: 0.32 days. Tom Jones and Bob Curbeam began the first STS-98 spacewalk from the ODS airlock on Atlantis, supervising the ISS/Destiny assembly operations. The airlock was depressurized at 1544 GMT. PMA-2 was berthed on Z1 at 1650 GMT; Destiny was unberthed from the payload bay at 1735 GMT and docked to Unity at 1900 GMT. At 1935 GMT Curbeam was connecting ammonia coolant lines when a leaking connector sprayed ammonia into space, contaminating his suit. He was ordered to stay in sunlight to bake off the ammonia. At around 2311 GMT the spacewalkers returned to the airlock, closing the hatch at 2318 GMT. A new depressurization for decontamination was begun at 2342 GMT, with the airlock fully depressurized at 2350 GMT. The hatch was then opened and closed quickly at 2351-2352 GMT, to flush the airlock of any ammonia residue. This last event was not counted as an EVA by NASA.
2001 February 12 -
  • NEAR, Asteroid Eros Landing Nation: USA. Spacecraft: NEAR. Periapsis of the orbit was as low as 24 km above the surface of the asteroid during its final days. At the end of its mission, NEAR touched down on the surface of Eros at 20:01:52 GMT on 12 February 2001. The spacecraft obtained 69 high-resolution images before touchdown, the final image showing an area 6 meters across. NEAR apparently came to rest with the camera and gamma-ray spectrometer pointing towards the ground and the solar panels and low gain antenna pointing generally towards the Earth and Sun. NEAR was not designed as a lander, but survived the low-velocity, low-gravity impact, a signal continued after the "landing" using the omni-directional low-gain antenna as a beacon.
2001 February 12 - 15:59 GMT -
  • EVA STS-98-2 Nation: USA. Program: ISS. Spacecraft: International Space Station. Crew: Jones, Curbeam. Flight: STS-98. EVA Duration: 0.28 days. STS-98 EVA-2 began at 1555 GMT on February 12 with depressurization of the airlock. The astronauts went to battery power at 1559 GMT. The PMA-2 docking port was attached to Destiny at 1728 GMT. The Power Data Grapple Fixture (PDGF) was removed from its location on an adaptive payload carrier on the port side of the payload bay (probably bay 5P) and installed on Destiny. The PDGF will be used by the Station's robot arm, and is an improved grapple fixture with electrical power and data ports. The hatch was closed at 2240 GMT and the airlock was repressurized at 2249 GMT
2001 February 12 - 16:28 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.187NM.
  • Microgravity mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi). References: 2.
2001 February 14 - 14:48 GMT -
  • EVA STS-98-3 Nation: USA. Program: ISS. Spacecraft: International Space Station. Crew: Jones, Curbeam. Flight: STS-98. EVA Duration: 0.23 days. On the third STS-98 EVA the airlock was depressurized at 1443 GMT, with hatch open at around 1445 and battery power at 1448. The spare SASA S-band antenna was unberthed from an adapter beam in the payload bay (around bay 4P?) and installed on Z1. The +X (starboard) TCS radiator on P6, launched on the previous mission, was deployed at 1649 GMT. The astronauts completed the spacewalk with repressurization of the airlock at 2013 GMT
2001 February 16 - 10:28 GMT - Launch Site: Barents Sea Launch Area. Launch Complex: -. Launch Pad: 69.5 N x 34.2 E. Launch Vehicle: R-29. Model: Shtil. LV Configuration: Shtil VMF RF.
  • Operational test Nation: Russia. Agency: VMF RF. Apogee: 1,000 km (600 mi). References: 2.
2001 February 16 - 10:43 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Topol. Model: Topol.
  • Operational test Nation: Russia. Agency: RVSN RF. Apogee: 1,000 km (600 mi). References: 2.
2001 February 20 - 08:48 GMT - Launch Site: Svobodniy. Launch Complex: LC5. Launch Pad: -. Launch Vehicle: Topol. Model: Start-1.
  • Odin Nation: Sweden. Mass: 250 kg (550 lb). Class: Astronomy. Type: Infrared. Spacecraft: Odin. Manufacturer: Swedish Space Corp. Agency: Swedish Space Corp. (Sweden). Perigee: 622 km (386 mi). Apogee: 622 km (386 mi). Inclination: 97.83 deg. COSPAR: 2001-007A. USAF Sat Cat: 26702. Sweden's Odin scientific satellite carried a submillimeter wave astronomy instrument and a radiometer for atmospheric studies. The 1.1-meter reflector fed 500 GHz and 119 GHz radiometers and was used to study galactic molecular clouds, complementing NASA's SWAS satellite. The Odin satellite was designed and built by the Swedish Space Corporation (Svenska Rymdbolaget or Rymdaktiebolaget). SSC does most of its satellite design and construction in-house, although Saab made the antenna and carried out satellite final assembly. SSC was a goverment-owned company and a contractor for the Rymdstyrelsen (Swedish National Space Board). References: 2, 296, 552, 554.
2001 February 20 - 18:58 GMT - Launch Site: Wake Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: SR19/SR19.
  • TCMP-3B Sensors mission Nation: USA. Agency: USA SSDC. Apogee: 300 km (180 mi). References: 2.
2001 February 20 -
  • Landing of STS-98 Nation: USA. Program: ISS. Flight: STS-98. STS-98 landed at 20:33 GMT.
2001 February 22 - 04:55 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.195DG.
  • J-PEX Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi). References: 2.
2001 February 25 - Launch Vehicle: KT. Model: KT-1.
  • Kaituozhe 1 Third Stage Engine Successfully Tested Nation: China. The solid engine used on the third stage of the Kaituozhe 1 launch vehicle performed its first ground test firing. The test was successful and all parameters meet design specifications. References: 424.
2001 February 26 - 08:09 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. LV Configuration: Soyuz 11A511U 670 / ISS-3P.
  • Progress M-44 Nation: Russia. Program: ISS. Payload: Progress M s/n 244. Mass: 7,250 kg (15,980 lb). Class: Manned. Type: Logistics. Spacecraft: Progress M. Manufacturer: RKK Energiya. Agency: RAKA. Perigee: 193 km (119 mi). Apogee: 243 km (150 mi). Inclination: 51.60 deg. COSPAR: 2001-008A. USAF Sat Cat: 26713. Duration: 49.22 days. Decay Date: 2001-04-16. Flight: ISS EO-1. ISS Servicing flight. Launch delayed from February10/20. Progress M-44 was a Russian, automatic cargo carrier that carried 2.5 tonnes of food, water, fuel, oxygen, and equipment to the International Space Station. In preparation for the docking, the ISS crew repositioned the Soyuz TM-31 escape craft from its port on Zvezda to a port on the Zarya module. Progress M-44 docked with the -Y port on Zvezda at 09:47 UT on 28 February. It undocked from Zvezda's aft port on April 16 at 0848 GMT and was deorbited at 1323 GMT over the Pacific Ocean. References: 2, 296, 552, 554.
2001 February 27 - 21:20 GMT - Launch Site: Cape Canaveral. Launch Complex: LC40. Launch Pad: SLC40. Launch Vehicle: Titan. Model: Titan 401B/Centaur. LV Configuration: Titan 401B/Centaur 4B-41/TC-22 (K-30).
  • USA 157 Nation: USA. Payload: Milstar-2 DFS 4. Mass: 4,670 kg (10,290 lb). Class: Communications. Type: Military. Spacecraft: Milstar. Manufacturer: Lockheed Martin Missiles & Space. Agency: USAF. Perigee: 35,764 km (22,222 mi). Apogee: 35,768 km (22,225 mi). Inclination: 4.50 deg. Period: 1,435.05 min. COSPAR: 2001-009A. USAF Sat Cat: 26715. Military Communications satellite. Launch delayed from October 30, December 14, 2000, and February 2 and February 24, 2001. The Milstar DFS 4 satellite (the second Milstar Block 2) provided secure communications for the US Department of Defense, with UHF, EHF and SHF band transmitters. Titan 4B-41 with core stage K-30 took off from Cape Canaveral and placed Milstar and the Centaur TC-22 upper stage in a suborbital trajectory. TC-22 then ignited to enter a 200 km parking orbit, and after two more burns delivered Milstar to geosynchronous drift orbit. Small engines on board the Milstar placed it at its targeted geostationary position. USA 157, a 4.5 tonne spacecraft, was the first in the Milstar 2 series which was capable of higher data rates and was more secure against disabling efforts. References: 2, 296, 552, 554.
2001 March 1 -
  • Discovery of NWA 856 Mars Meteorite Nation: Morocco.
2001 March 1 -
  • Discovery of NWA 856, 1669, 1950 Mars Meteorites Nation: Morocco.
2001 March 8 - Launch Site: Kourou. Launch Complex: ELA3. Launch Pad: -. Launch Vehicle: Ariane 5. Model: Ariane 5G. LV Configuration: Ariane 5G V140 (509).
  • Eurobird Nation: Europe. Payload: Eutelsat W1R. Mass: 3,050 kg (6,720 lb). Class: Communications. Spacecraft: Spacebus 3000. Manufacturer: Alcatel Space. Agency: Eutelsat. Perigee: 35,773 km (22,228 mi). Apogee: 35,798 km (22,243 mi). Inclination: 0.00 deg. Period: 1,436.00 min. COSPAR: 2001-011A. USAF Sat Cat: 26719. Launch delayed from March 2. Eurobird was a Spacebus 3000B3 built by Alcatel (Cannes). It was the 18th member of the European Eutelsat consortium's geosynchronous constellation and carried 24 Ku-band transponders to provide broad bandwidth and high power direct-to-home transmissions to enable digital entertainment and internet connections. The three tonne (with fuel) satellite was to be parked over 28.5 deg-E longitude, replacing the aging Copernicus (Kopernikus (DFS 3), 1992-066A). Dry mass was probably around 1300 kg. The satellite had an Astrium S400 bipropellant engine. Positioned in geosynchronous orbit at 28 deg E in 2001 As of 4 September 2001 located at 28.50 deg E drifting at 0.005 deg W per day. As of 2007 Mar 11 located at 28.52E drifting at 0.000W degrees per day. References: 2, 552, 554.
  • BSAT-2a Nation: Japan. Program: BSAT. Mass: 3,050 kg (6,720 lb). Class: Communications. Spacecraft: Star bus. Manufacturer: Alcatel Space. Agency: BSAT. Perigee: 35,764 km (22,222 mi). Apogee: 35,807 km (22,249 mi). Inclination: 0.10 deg. Period: 1,436.10 min. COSPAR: 2001-011B. USAF Sat Cat: 26720. BSAT-2a was a Japanese geosynchronous communications spacecraft and the second Orbital STAR-class television broadcasting satellite. Its launch mass was 1317 kg; dry mass was 535 kg. The satellite had a Thiokol Star 30CBP solid apogee motor. The new BSTAR STAR-class satellites are a new design replacing the earlier Starbus type satellite of which only one (Cakrawarta 1) was launched. BSAT Corp. (Broadcasting Satellite System Corp.) earlier launched HS-376 satellites BSAT 1a and 1b, replacing the government's BS series which began Japanese direct broadcast services in 1978. The satellite was to be parked over 110 deg-E longitude to provide direct-to-home voice, video and internet communications. Positioned in geosynchronous orbit at 110 deg E in 2001 As of 5 September 2001 located at 109.82 deg E drifting at 0.018 deg W per day. As of 2007 Mar 11 located at 109.92E drifting at 0.009W degrees per day. References: 2, 552, 554.
2001 March 8 - 11:42 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39B. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-102.
  • STS-102 Nation: USA. Program: ISS. Payload: Discovery F29. Class: Manned. Type: Spaceplane. Spacecraft: Discovery. Manufacturer: Boeing. Agency: NASA JSC. Perigee: 370 km (220 mi). Apogee: 381 km (236 mi). Inclination: 51.50 deg. Period: 92.06 min. COSPAR: 2001-010A. USAF Sat Cat: 26718. Duration: 12.83 days. Decay Date: 2001-03-21. Crew: Wetherbee, Kelly, Voss, Helms, Thomas Andrew, Richards Paul, Usachyov. Flight: STS-102, ISS EO-2. STS 102 was an American shuttle spacecraft that carried a crew of seven astronauts (six American and one Russian). The primary mission was to deliver a multi-rack Italian container (Leonardo MultiPurpose Logistics Module, LMPLM) to the Destiny Module of the International Space Station, ISS. It docked with the ISS at 05:34 UT on 9 March. The 6.4 m x 4.6 m cylindrical LMPLM delivered new equipment to Destiny, and retrieved used/unwanted equipment, and trash back to the shuttle. The crew did a few spacewalks to install a platform on the ISS to support a Canadian robot arm when it arrives next month. The STS 102 left behind three of the astronauts (two American and one Russian) and brought back the three astronauts (one American and two Russian) who had been inhabiting the ISS for about four and a half months. It landed at Cape Canaveral at 07:31 UT on 21 March.

    Discovery was launched on mission STS-102 (Space Station flight 5A.1) into an initial 60 x 222 km x 51.6 deg orbit. The mission was delivery of supplies and equipment, and changeout of the Expedition One and Expedition Two station crews. STS-102 carried the Leonardo Multi Purpose Logistics Module (MPLM), built by Alenia Spazio (Torino), to the International Space Station. The 6.4 m x 4.6 m cylindrical MPLM was a descendant of the Spacelab long modules. Also carried was a Spacehab/Energia unpressurized Integrated Cargo Carrier with LCA/MTSAS-A, RU, and PFCS. A sidewall adapter beam with two GAS canisters (G-783 and WSVFM) was also on board. WSVFM measured vibration during launch. Another adapter beam, probably at the rear of the payload bay, carried SEM-9. SEM-9 and G-783 contained high school microgravity experiments.

    Leonardo carried 16 'racks' of equipment, including the Human Research Facility Rack (Rack 13) which allowed the astronauts to do extensive medical experiments, the CHeCS Rack (28), the DDCU-1 and DDCU-2 racks (7 and 9), the Avionics-3 (Rack 6), and the MSS Avionics/Lab (Rack 11) and Avionics/Cupola (Rack 12) racks for a total of 7 equipment racks to be installed on Destiny. Three Resupply Stowage Racks (50, 51, 52) and four Resupply Stowage Platforms (180, 181, 182 and 188) remained installed on Leonardo, with their equipment bags being individually transferred to the Station. System Racks 2, 3, 4, 5 and 8 were already on Destiny together with stowage racks 110 through 117. Each rack had a mass of 150-300 kg.

    The orbiter fired its OMS engines at 1221 GMT to raise the orbit to 185 x 219 km. Discovery docked with the PMA-2 port on the Station at 0639 GMT on March 10. The LCA (Lab Cradle Assembly) was attached to Destiny's +Z side during an EVA. It was to be used on the next mission to temporarily place a Spacelab pallet on Destiny during installation of the Station's robot arm. Later, it would be the site for the main Station truss, beginning with segment S0.

    The PMA-3, on Unity at the -Z nadir position, had to be moved to the port position to make room for Leonardo. An external stowage platform was attached to Destiny and the External Stowage Platform and the PFCS Pump Flow Control System were added to the port aft trunnion on Destiny. A rigid umbilical (RU) was connected to the PDGF grapple fixture on Destiny to support the Station's future robot arm. Leonardo was docked to Unity at -Z for a while so that its cargo could be transferred to the station easily; it was then be returned to the payload bay and brought back to earth.

    At 0232 GMT on March 19 command of ISS was transferred to Expedition 2 and the hatches were closed. Discovery undocked at 0432 GMT and flew once around the station before departing at 0548 GMT. ISS mass after undocking was 115527 kg. The OMS engines fired for the deorbit burn at 0625 GMT on March 21, and Discovery touched down on runway 15 at Kennedy Space Center at 0731 GMT. References: 2, 552, 554.

2001 March 11 - 05:12 GMT -
  • EVA ISS EO-2-1 Nation: USA. Program: ISS. Spacecraft: International Space Station. Crew: Voss, Helms. Flight: ISS EO-2. EVA Duration: 0.37 days. On March 11 Jim Voss and Susan Helms made a spacewalk from Discovery's airlock. A PAD device used to attach equipment to the RMS arm floated free and Voss retrieved a spare one from Unity, putting the walk behind schedule. The astronauts installed the Lab Cradle Assembly and the Rigid Umbilical on Destiny and disconnected the umbilicals connecting the PMA-3 docking port to Unity. The astronauts then spent two-and-a-half hours back in the depressurized airlock in case their help was needed during the move of PMA-3. Thomas used the RMS arm to unberth PMA-3 from the nadir port on Unity and relocated it to the port port location, freeing up the nadir for the MPLM. The airlock was depressurized at 0508 GMT and repressurized at 1408 GMT.
2001 March 13 - 05:23 GMT -
  • EVA STS-102-1 Nation: USA. Program: ISS. Spacecraft: International Space Station. Crew: Thomas Andrew, Richards Paul. Flight: STS-102. EVA Duration: 0.26 days. The airlock was depressurized at 0518 GMT and the hatch opened at 0520 GMT. The astronauts took the External Stowage Platform from the ICC carrier to the port side of the Destiny module, and then installed the spare Pump Flow Control System on it. The ESP was used to store on-orbit-spare equipment. Next they hooked up cables on the robot arm's umbilical, and travelled up to the top of the P6 tower to fix a solar array latch - it just needed a good thump - and inspect the FPP experiment. The astronauts returned to the airlock at 1132 GMT and began repressurizing at 1144 GMT.
2001 March 18 - Launch Site: Kiritimati. Launch Complex: -. Launch Pad: 0.0 N x 154.0 W. Launch Vehicle: Zenit. Model: Zenit-3SL.
  • XM-2 Rock Nation: USA. Mass: 4,666 kg (10,286 lb). Class: Communications. Spacecraft: HS 702. Manufacturer: Boeing Satellite Systems. Agency: XM Radio. Perigee: 35,785 km (22,235 mi). Apogee: 35,788 km (22,237 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2001-012A. USAF Sat Cat: 26724. The XM Radio satellites (using Boeing 702 buses) provided digital radio entertainment broadcast to the US. The XM-2 Rock satellite was accompanied by the XM-1 Roll spacecraft launched later in 2001. A Boeing Sea Launch Zenit-3SL took off from the Odyssey floating launch platform at 154W 0 N in the Pacific. The two-stage Zenit put the Blok DM in a suborbital trajectory with a 190 km apogee; the DM first burn went to a 180 x 990 km x 1.3 deg orbit, with the second burn delivering Rock to geostationary transfer orbit. The 4.7 tonne (with fuel), 18 kW satellite carried two transmitters (3 kW each) in the S-band to relay 100 channels of digital quality music uplinked in the X-band from one or more ground stations. It was parked over 114.9 deg-W longitude. The investors include several auto manufacturers who were to be equipping the special receivers in their models. As of 4 September 2001 located at 114.98 deg W drifting at 0.001 deg W per day. As of 2007 Mar 10 located at 115.14W drifting at 0.003W degrees per day. References: 2, 552, 554.
2001 March 19 - Launch Site: Kodiak. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aries. LV Configuration: Aries QRLV-1.
  • Target mission Nation: USA. Agency: USAF SMC. Apogee: 163 km (101 mi). References: 2.
2001 March 21 - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: MT-135. Model: MT-135. LV Configuration: MT-135 R1119.
  • Last flight Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 55 km (34 mi). The Japan Meteorological Agency launched the 1119th MT-135P meteorological sounding rocket from the meteorological observation station in Sanriku-cho, Iwate-ken. This was the final launch of the type. The MT-135P had served for more than thirty years gathering meteorological data in the upper atmosphere since the first launching on July 15, 1970. IHI Aerospace Co., Ltd. has been responsible for design, development and manufacture of the MT-135P. References: 2.
2001 March 21 -
  • Landing of STS-102 Nation: USA. Program: ISS. Flight: STS-102, ISS EO-1. STS-102 landed at 07:31 GMT with the crew of Wetherbee, Kelly, Thomas Andrew, Richards Paul, Gidzenko, Krikalyov and Shepherd aboard.
2001 March 23 -
  • Mir deorbited Nation: Russia. Program: Mir. Spacecraft: Mir. On March 19, 2001 Mir was in a 224 x 230 km x 51.6 deg orbit. On March 23 at 0033 GMT Progress M1-5 carried out the first small DPO burn to lower Mir's orbit from 212 x 218 km to 190 x 219 km. A second small burn began at 0201 GMT and put Mir in a 150 x 215 km orbit. The main deorbit burn began at 0507 GMT, lowering perigee to less than 80 km. At 0550 GMT observers in Fiji reported seeing multiple bright reentry bodies passing overhead, confirming that the station had broken up by that time. The impact zone was around 160 W 40 S.
2001 March 31 - Launch Site: Fort Wingate. Launch Complex: LC96. Launch Pad: -. Launch Vehicle: Hera. LV Configuration: Hera 19/MBRV-3.
  • MBRV-3/PAC-3 DT-8a Target mission Nation: USA. Agency: USA SSDC. Apogee: 114 km (70 mi). References: 2.
2001 March 31 - 06:00 GMT - Launch Site: Balasore. Launch Complex: -. Launch Pad: -. Launch Vehicle: Prithvi. LV Configuration: Prithvi 18.
  • Solid fuel test Nation: India. Agency: IDRDL. Apogee: 100 km (60 mi). References: 2.

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