Health: Again To Basics

Inclination: 45.10 deg. Interval: 3,808.60 min. Inclination: 51.30 deg. Period: 89.71 min. Inclination: 51.60 deg. Period: 92.20 min. The payload bay doors were closed at 04:14 GMT on September 20 and at 06:50 GMT the OMS engines ignited for a three minute burn reducing the orbit from 374 x 386 km x 51.6 deg to 22 x 380 km x 51.6 deg. The ultimate separation burn was executed about 45 minutes after undocking. At Oct 12 on 03:01 GMT the NC1 burn raised the orbit to 180 x 349 km; NC3 on Oct 12 to 311 x 375 km;. Perigee: 563 km (349 mi). Perigee: 386 km (240 mi). Perigee: 382 km (237 mi). Perigee: 226 km (140 mi). COSPAR: 2000-078A. Apogee: 365 km (226 mi). COSPAR: 1999-040A. Apogee: 280 km (170 mi). Discovery undocked from ISS at 22:39 GMT on June three right into a 385 x 399 km x 51.6 diploma orbit, leaving the station with out a crew aboard.

Endeavour docked with the Station’s PMA-three docking port at 1959 GMT on December 2. Astronauts then put in the P6 solar panel truss to the station during a sequence of spacewalks. 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 had been referred to as off because of persistent wind issues at Kennedy Space Middle. Repressurisation began at 21:22 GMT for a duration of 7 hours 07minutes. Leroy Chiao and Bill McArthur started the third STS-92 EVA at 15:30 GMT on October 17, completing their work at 22:18 GMT for a total time of 6 hours forty eight minutes. They rode the RMS arm up to Zvezda and started putting in cables, reaching a distance of 30 meters from the airlock when installing Zvezda’s magnetometer. In all, they spent 7 days, 21 hours and 54 minutes docked to the International Space Station, outfitting the brand new Zvezda module for the arrival of the Expedition One crew later this fall. The automobile landed on RW15 at Kennedy Area Middle at 06:20 GMT. After some problems arduous dock was achieved at 02:48 GMT. Good major care may help prevent any health problems from escalating. Hubble Space Telescope (HST) servicing mission SM-3A, delayed repeatedly by technical issues with the shuttle fleet after the near-disastrous previous launch. Columbia landed at 03:20 GMT on July 28 on runway 33 at Kennedy Space Center.

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 transferred tools from the Spacehab Logistics Double Module in the payload bay to the inside of the station. Atlantis closed its payload bay doors round 02:30 GMT on May 29. Fired the OMS engines for deorbit at 05:12 GMT. Payload: Atlantis F22. Mass: 115,900 kg (255,500 lb). Payload: Endeavour F13. Mass: 116,277 kg (256,346 lb). Payload: Discovery F28. Mass: 115,127 kg (253,811 lb). STS-ninety two – . Call Sign: Discovery. Type: Manned spaceplane. Flight: STS-92. Sort: Manned spaceplane. Flight: STS-96. Type: Manned spaceplane. Flight: STS-98. Type: Manned spaceplane. Flight: STS-106. STS-106 – . Call Sign: Atlantis. Crew: Cockrell, Curbeam, Ivins, Jones, Polansky. Nation: USA. Related Persons: Cockrell, Curbeam, Ivins, Jones, Polansky. Nation: USA. Related Persons: Ashby, Coleman, Catherine, Collins, Eileen, Hawley, Tognini. Nation: USA. Related Persons: Helms, Kelly, James, Richards, Paul, Thomas, Andrew, Usachyov, Voss, Wetherbee.

Nation: USA. Related Persons: Halsell, Helms, Horowitz, Usachyov, Voss, Weber, Mary, Williams, Jeffrey. Crew: Halsell, Helms, Horowitz, Usachyov, Voss, Weber, Mary, Williams, Jeffrey. Crew: Gorie, Kavandi, Kregel, Mohri, Thiele, Voss, Janice. Crew: Altman, Burbank, Lu, Malenchenko, Mastracchio, Morukov, Wilcutt. Crew: Ashby, Coleman, Catherine, Collins, Eileen, Hawley, Tognini. Z1 carried the control second gyros, the S-band antenna, and the Ku-band antenna. The crew additionally tested the four 290-kg gyroscopes in the truss, known as Control Moment Gyros, which might be used to orient the ISS as it orbits the Earth. It was to perform as a science and know-how module and the primary control module for the ISS. They fired response control system jets in a sequence of pulses of 1.4 seconds each, over a 30-minute period, gently elevating the station’s orbit by about 3.1 km. Launch came the subsequent day, with Endeavour entering an preliminary 75 km x 313 km x 51.6 degree orbit. Because of this, the crew’s last departure from the Station’s Unity module was delayed. The main mission was to put in a 72 m x 11.Four m, 65 kW double-wing solar panel on the Unity module of the ISS. The principle engines cutoff at 10:19 GMT.