Jonathan's Space Report No. 448 2001 Mar 4, Cambridge, MA ------------------------------------------------------------------------------- Shuttle and Stations -------------------- Atlantis landed at Edwards AFB on Feb 20, completing mission STS-98. Plans to land on Feb 18 and Feb 19 were called off due to bad weather at Kennedy Space Center. The deorbit burn was at 1927 UTC 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 UTC and touchdown on runway 22 was at 2033 UTC. On Mar 1 Atlantis was flown on the back of NASA's SCA 911 carrier aircraft to Altus AFB, Oklahoma and will be returned to KSC when the weather clears. Meanwhile, in nearby Palmdale, Columbia has completed its maintenance period and began its journey back to KSC on NASA SCA 905 half an hour earlier, landing at Dyess AFB, Abilene, Texas. There are two converted Boeing 747 Shuttle Carrier Aircraft, but it's been a while since both have been needed at the same time and this is the first time that both have been in the air carrying an Orbiter simultaneously. Soyuz TM-31, carrying the Expedition One crew of Shepherd, Gidzenko and Krikalyov, undocked from the -Y port on Zvezda on Feb 24 at 1006 UTC and redocked with the -Z port on Zarya at 1037 UTC. This freed the Zvezda port for a Progress resupply ship. Progress No. 244 was launched on Feb 26 and named Progress M-44 once on orbit. Launch vehicle was a Soyuz 11A511U, which took off from GIK-5 (Baykonur). Progress M-44 docked with the -Y port on Zvezda at 0950 UTC on Feb 28. The next Shuttle launch is STS-102, which will carry the Leonardo Multi Purpose Logistics Module (MPLM), built by Alenia Spazio (Torino). The MPLM is a descendant of the Spacelab long modules. Also carried is a Spacehab/Energia unpressurized Integrated Cargo Carrier with LCA/MTSAS-A, RU, and PFCS (An ammonia servicing system has reportedly been omitted from the cargo). A sidewall adapter beam with two GAS canisters (G-783 and WSVFM) is also on board. WSVFM measures vibration during launch. Another adapter beam, probably at the rear of the payload bay, carries SEM-9. SEM-9 and G-783 contain high school microgravity experiments. I'm guessing that the ICC is probably in Bay 5 with the MPLM behind it in Bay 8-12, and SEM-9 the adapter beam in bay 13, but NASA does not seem to have released any photos or diagrams of the overall STS-102 cargo bay. The robot arm carried on Discovery is RMS 301, according to Bill Harwood's info on the spaceflightnow.com site. Discovery will dock at PMA-2 on Destiny. The LCA (Lab Cradle Assembly, apparently the same thing as MTSAS-A, Module Truss Structure Attachment System) will be attached to Destiny's +Z side during an EVA. It will be used on the next mission to temporarily place a Spacelab pallet on Destiny during installation of the Station's robot arm. Later, it will be the site for the main Station truss, beginning with segment S0. The PMA-3, currently on Unity at the -Z nadir position, will be moved to the port position to make room for Leonardo. An external stowage platform will be attached to Destiny and the External Stowage Platform and the PFCS Pump Flow Control System will be added to the port aft trunnion on Destiny. A rigid umbilical (RU) will be connected to the PDGF grapple fixture on Destiny to support the Station's future robot arm. Leonardo will be docked to Unity at -Z for a while so that its cargo can be transferred to the station easily; it will then be returned to the payload bay and brought back down. STS-102 cargo: The JSR guess Est. Mass (kg) Bay 1-2: Orbiter Docking System 1800 and External Airlock 3 EMU spacesuits (S/N unknown) 360? Bay 4 Port?: Adapter Beam with 218? WSVFM and G-782 Bay 5?: Integrated Cargo Carrier (ICC) 1282 with LCA (Lab Cradle Assembly) 83 (MTSAS-A) ESP (External Stowage Plat.)+ PFCS (Pump Flow Control System) 210 RU (Rigid Umbilical) 28 Bay 8-12?: Leonardo Module (MPLM-1) 4760 MPLM racks and cargo 5362 Bay 13S? Adapter Beam with SEM-09 100? Unknown Adapter Beam with 100? Assembly Power Converter Units? Sill: Canadarm RMS 301 410 ------ Total payload bay cargo 14713 kg Leonardo carries 16 'racks' of equipment, including the Human Research Facility Rack (Rack 13) which will allow 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) will remain installed on Leonardo, with their equipment bags being individually transferred to the Station. System Racks 2, 3, 4, 5 and 8 are already on Destiny together with stowage racks 110 through 117. Each rack has a mass of around 150-300 kg. The STS-102 crew are Jim Wetherbee (commander), James Kelly (pilot), Andrew Thomas and Paul Richards (mission specialists). In addition, Discovery will carry the Expedition Two crew of Yuriy Usachyov, James Voss and Susan Helms to the Station and bring back the Expedition One crew. The International Space Station was in a 373 x 384 km x 51.6 deg orbit on Mar 2. The Mir complex was in a 253 x 269 km x 51.6 deg orbit on Mar 3, with deorbit expected within the next two weeks. Recent Launches --------------- Sweden's Odin scientific satellite was launched on Feb 20 by a Russian Start-1 rocket from the 2 GIK spaceport at Svobodniy. The Start-1 is a modified Topol'-class ICBM. Odin carries a submillimeter wave astronomy instrument and a radiometer for atmospheric studies. The 1.1-meter reflector feeds 500 GHz and 119 GHz radiometers and will be 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. Although SSC is usually the public face of the Swedish space program, technically it is a goverment owned company and is a contractor for the actual space agency, the Rymdstyrelsen (Swedish National Space Board). The four-stage solid Start-1 entered a 576 x 606 km x 97.8 deg orbit about 8 minutes after launch A post-boost engine attached to the fourth stage then raised the orbit to 610 x 621 km. I thought this was a liquid engine, but Sven Grahn informs me that it is actually a solid-propellant gas generator with multiple nozzles. A similar system was used in the Aeronutronic-Ford Trident upper stage used on a number of Atlas reentry tests in the late 1960s (and if anyone has info on *that* interesting and poorly documented vehicle, please get in touch!). A number of debris objects have been cataloged between the initial and final orbits. The Milstar DFS 4 satellite (the second Milstar Block 2) was launched on Feb 27. Milstar provides 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 will place it at its targeted geostationary position. Milstar is built by Lockheed Martin Missiles and Space (Sunnyvale); Titan Centaur is built by Lockheed Martin Astronautics (Denver). The Japanese Asuka (ASTRO D, ASCA) X-ray astronomy satellite reentered on Mar 2. It operated from Feb 1993 to Jul 2000 and made observations of the hard X-ray sky with CCD imagers and a foil-type set of X-ray telescopes. Table of Recent Launches ----------------------- Date UT Name Launch Vehicle Site Mission INTL. DES. Jan 9 1700 Shenzhou 2 ) Chang Zheng 2F Jiuquan Spaceship 01A SZ-2 Orb. module) Science 01C Jan 10 2209 Turksat 2A Ariane 44P Kourou ELA2 Commsat 02A Jan 24 0428 Progress M1-5 Soyuz-U Baykonur LC1 Cargo 03A Jan 30 0755 Navstar GPS 54 Delta 7925 Canaveral SLC17A Navsat 04A Feb 7 2306 Sicral ) Ariane 44L Kourou ELA2 Commsat 05A Skynet 4F ) Commsat 05B Feb 7 2313 Atlantis (STS-98))Space Shuttle Kennedy LC39A Spaceship 06A Destiny ) Module 06B Feb 20 0848 Odin Start-1 Svobodniy Astronomy 07A Feb 26 0809 Progress M-44 Soyuz-U Baykonur LC1 Cargo 08A Feb 27 2120 Milstar DFS 4 Titan Centaur Canaveral SLC40 Commsat 09A Current Shuttle Processing Status _________________________________ Orbiters Location Mission Launch Due OV-102 Columbia Dyess AFB STS-107? Late 2001? OV-103 Discovery LC39B STS-102 2001 Mar 8 ISS 5A.1 OV-104 Atlantis Altus AFB STS-98 2001 Feb 7 ISS 5A OV-105 Endeavour OPF Bay 2 STS-100 2001 Apr 19 ISS 6A LC39B: Mobile Launch Platform 3 (MLP-3) Solid Rocket Boosters BI-106/RSRM-78 External Tank ET-107 Orbiter OV-103 (Discovery) .-------------------------------------------------------------------------. | Jonathan McDowell | phone : (617) 495-7176 | | Harvard-Smithsonian Center for | | | Astrophysics | | | 60 Garden St, MS6 | | | Cambridge MA 02138 | inter : jcm@cfa.harvard.edu | | USA | jmcdowell@cfa.harvard.edu | | | | JSR: http://hea-www.harvard.edu/~jcm/space/jsr/jsr.html | | Back issues: http://hea-www.harvard.edu/~jcm/space/jsr/back | | Subscribe/unsub: mail majordomo@head-cfa.harvard.edu, (un)subscribe jsr | '-------------------------------------------------------------------------'