Jonathan's Space Report No. 534 2004 Sep 8, Somerville, MA ------------------------------------------------------------------------------- * Fred Whipple Fred Whipple died on August 30 at the age of 97. Fred was a pioneer of the Space Age. He discovered his first comet in 1932; invented radar chaff countermeasures in World War II; suggested the `Whipple Shield' meteoroid bumpers now used on spacecraft in 1946; and developed the now-accepted 'dirty snowball' theory of comets in 1950. He was director of the Smithsonian Observatory (SAO) from 1955-1973 and led American optical tracking of Sputnik and the other early satellites. The Moonwatch program made SAO known worldwide as a source of information on satellites. Fred was scientifically active well into his 90s. Although after a bicycle accident when he was 89 he had stopped cycling into work, we often saw the car with the 'COMETS' licence plate parked outside. In recent years he was a member of the Contour comet mission science team. Fred arrived at Harvard (where SAO is now located) in 1931; he cleared out his office only a few weeks ago and was still mentally sharp although physically frail. Fred was also well known for his sense of humour and approachability; we will miss him. * Nemesis for Genesis On Sep 8 the Genesis space probe became the first artifact to return from beyond lunar orbit to the Earth's surface. Unfortunately, the parachute system failed to deploy and the capsule hit the Utah desert at high speed. The capsule is embedded in the desert floor and is split open; it is not yet clear to what extent the solar wind samples have been ruined. After targeting maneuvers on Aug 9, Aug 29, and Sep 6, the Genesis Sample Return Capsule (SRC) separated from the Genesis spacecraft at around 1153 UTC on Sep 8, 66000 km above the Earth. At 1215 UTC the spacecraft made a small separation burn, burning up over the Pacific at around 1550 UTC. At 1555 UTC the SRC entered the atmosphere over Oregon at about 11 km/s (Earth-relative) and an angle of 8.25 degrees below the horizontal, giving an orbital perigee close to zero and an apogee around 1.5 million km. The SRC's heat shield protected it through atmospheric entry. A mortar which was intended to release the drogue parachute at 33 km high failed to fire and at 1558 UTC the tumbling SRC impacted the Dugway Proving Ground at the Utah Test and Training Range at 40 07 40N 113 30 29W. Impact velocity was around 40 to 90 m/s, over 200 times slower than it was travelling a few minutes earlier but still more than enough to wreck the vehicle. * Space Station Astronauts Padalka and Fincke made a spacewalk on Sep 3 from the Pirs airlock module using Orlan suits M-25 and M-26. The Pirs was depressurized by 1621 UTC; hatch open was at 1643 UTC and hatch close at 2204 UTC with repressurization beginning at 2206 UTC for a total of 5hr 46min of depressurization time. They installed equipment on the Zarya and Zvezda modules. (Thanks once again to Andrey Krasil'nikov for timing data). The old 70 kg Zarya PIG container with the RRZh1 flow regular valve panel, removed at 1729 UTC, was jettisoned during the EVA at 2151 UTC. Three more antennas were installed on Zvezda for rendezvous operations with the European ATV cargo ship; five antenna covers were ejected at around 2100 UTC, and at least two cleaning towels were jettisoned at 2110 UTC. A total of five objects have been cataloged by Space Command, at least one of which is probably the container. * Chinese satellite A new Chinese recoverable satellite was launched on Aug 29 by a CZ-2C rocket from the Jiuquan Space Center into a 165 x 490 km x 63.0 deg orbit. The satellite is one of the FSW series, and is expected to return a capsule to Earth after 27 days in space. I'm a bit surprised that it used the CZ-2C rather than the beefed-up CZ-2D which was used for the last three FSW launches. The CZ-2C was used for the older FSW-1 model, rather than the more modern FSW-2 and JB-4 models. However, Chen Lan has suggested that this CZ-2C is one of the stretched ones left over from the Iridium program, and may have a larger payload capacity. The new launch has the highest apogee of any FSW series flight; the satellite has not yet been given an official name by China. * Israeli launch failure The 'Ofeq-6 spy satellite failed to reach orbit on Sep 6. According to the Jerusalem Post, the third stage of the Shavit launch vehicle failed to operate and the payload fell in the Mediterranean. The launch time was reported as 1:53pm local, which I believe corresponds to 1053 UTC. The lower two stages separated and at 1102 UTC and 260 km high the AUS-51 third stage was meant to fire for 92s to put the satellite in a retrograde 260 x 770 km x 143.5 deg orbit. (Most countries launch east to gain energy from the Earth's rotation; Israel launches west over the Med to avoid misunderstandings with its eastern neighbours.) Without the third stage burn, the vehicle was probably in a roughly -5700 x 260 km orbit and would have impacted around 1106 UTC, probably somewhere south of Crete. * Atlas Centaur IIAS AC-167 AC-167, the final Lockheed Martin Atlas IIAS, was launched on Aug 31 at 2317 UTC, placing a classified National Reconnaissance Office payload in an elliptical orbit of around 400 x 40000 km x 63 deg at 0030 UTC on Sep 1. The payload is probably a communications satellite used to relay data from imaging spy satellites. The Centaur upper stage dumped its remaining fuel around 0100 UTC, creating a cloud which was spotted by amateur observers. The launch was given the codename NROL-1, and the USA 179 satellite is the second elliptical orbit NRO Atlas launch, following USA 137 in Jan 1998. Two geostationary NRO Atlas launches, in Dec 2000 and Oct 2001, might be part of the same data relay satellite series. There were two unusual things about the Atlas missile, first launched in 1957, at which time it was a product of Convair/San Diego (later GD/Astronautics, later Martin Marietta, finally LockMart; production was moved to the old Martin Titan plant in Denver during the 1990s). One was the stage-and-a-half construction of the MA-1 propulsion system (whose more recent versions were designated MA-2, MA-3 and finally today's MA-5), in which common propellant tanks were used to feed three engines, two of which were in a 'booster package' jettisoned two minutes into flight (this was actually only a dummy system in the 1957 Atlas A launches, and was first used for real on Atlas B in 1958). This gave high initial thrust, and let you get rid of some heavy machinery early on; the Atlas main 'sustainer' stage could reach orbit with a significant payload, as it did on Mercury missions like John Glenn's. The second unusual thing was the `balloon tank' of the sustainer stage. The stage has a very thin wall and must be kept pressurized at all times - using nitrogen when the stage isn't fuelled - or else it will crumple under its own weight, folding in half with spectacularly unwanted results (and indeed this was demonstrated on a couple of occasions.) Today was the last flight of the MA-5 stage-and-a-half propulsion system. There is one more flight scheduled for the balloon tank, AC-206 in January - this Atlas 3 uses a Russian RD-180 engine instead of the MA-5, but still has many elements of the traditional Atlas. The Atlas 5 now coming into service is really a completely different vehicle, with neither booster package nor balloon tank. Table of Recent Launches ----------------------- Date UT Name Launch Vehicle Site Mission INTL. DES. Aug 3 0616 MESSENGER Delta 7925H Canaveral SLC17B Probe 30A Aug 4 2232 Amazonas Proton-M/Briz-M Baykonur LC200/39 Comms 31A Aug 11 0503 Progress M-50 Soyuz-U Baykonur LC1 Cargo 32A Aug 29 0750 FSW CZ-2C Jiuquan Imaging 33A Aug 31 2317 USA 179 (NROL-1) Atlas IIAS Canaveral LC36A Comms? 34A Sep 6 1053 'Ofeq-6 Shaviyt Palmachim Imaging F01 .-------------------------------------------------------------------------. | Jonathan McDowell | phone : (617) 495-7176 | | Somerville MA 02143 | inter : jcm@host.planet4589.org | | USA | jcm@cfa.harvard.edu | | | | JSR: http://www.planet4589.org/jsr.html | | Back issues: http://www.planet4589.org/space/jsr/back | | Subscribe/unsub: mail majordomo@host.planet4589.org, (un)subscribe jsr | '-------------------------------------------------------------------------'