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PicoSAT Launch date September 30, 2001 Carrier rocket Athena I Launch site Kodiak Launch Complex, Kodiak, AK Orbital elements Inclination 100.2° Repeat interval 100.7 min PicoSAT, launched on September 30, 2001, is a real time tracking satellite picosatellite of the miniaturized satellite series. The name "PICO" combines the first letters of all four of its experiments (see below). PICOSat series are designed for a minimum of one year of on-orbit operations. The current Picosat 9 is a British-built (US DOD-funded) microsatellite (67 kg) to test electronic components/systems in space conditions. Oboard this model carries four test payloads: Polymer Battery Experiment (PBEX), Ionospheric Occultation Experiment (IOX), Coherent Electromagnetic Radio Tomography (CERTO) and On Orbit Mission Control (OOMC) an ultra-quiet platform (OPPEX). PICOSat flies in a 800 km circular orbit with a 67 degree inclination. PICOSat uses a gravity gradient boom for stabilization. The body mounted solar panels produce an average on orbit power of 22 W. The Ultra-Quiet Platform (UQP), developed by the US Air Force Research Lab, aims to provide a 10:1 reduction in vibration isolation over a 100 Hz bandwidth between the spacecraft bus and a science payload.[1] Contents 1 Early versions 2 PicoSat specifications 2.1 PicoSat 1 & 2 (tethered) 2.2 PicoSat 9 2.3 Identifications 3 See also 4 References 5 Further reading 6 External links Early versions Tethered Picosats, Picosat 5, Picosat 6, Picosat 7, and Picosat 8 are hectogram mass satellites that were ejected from OPAL (2000-004C). The primary builders were by engineering students at Santa Clara University in California. They used off-the-shelf components and miniature batteries, for technology tests. The Tethered Picosats were a pair of Picosats tethered together by a short wire, was ejected on February 8, 2000, from a OPAL Launch System[2]. Picosats 7 and 8 on launched on 11 February, and Picosats 5 and 6 launched on 12 February. Alternate common names were given by the investigators: Picosats 7 and 8 are the Thelma and Louise pair and Picosats 5 and 6 are the JAK and Stensat pair. The Tethered Picosats were functional for a short time after ejection, communicating with each other by microwatt radio transmitters. There was no indication if the Picosats (5, 6, 7,and 8) were operational at the time of ejection into orbit. USSPACECOM's Picosat numbers extending to eight is erroneous. There were only six Picosats on board the OPAL, with possible one or two still on the ground, with tests to communicate with the orbiters. The tests were managed by the Defense Advanced Research Project Agency (DARPA). [3] PicoSat specifications PicoSat 1 & 2 (tethered) NORAD ID: 26080 Int'l Code: 2000-004H Perigee: 741.4 km Apogee: 788.1 km Inclination: 100.2° Period: 100.0 min Launch date: January 27, 2000 Source: United States (US)[4] Launch vehicle: Minotaur Launch site: Vandenberg Air Force Base.[5] PicoSat 9 NORAD ID: 26930 Int'l Code: 2001-043B Perigee: 791.0 km Apogee: 806.5 km Inclination: 67.0° Period: 100.7 min Launch date: September 30, 2001 at 02:40:00 UTC[6] Source: United States (US)[4] Launch Vehicle: Athena I Launch Site: Kodiak Launch Complex [1] Identifications International designation numbers with USSPACECOM Catalog numbers are in parentheses:[7] 2000-004H (26080) Picosat 1/2 2000-004J (26091) Picosat 5 2000-004K (26092) Picosat 6 2000-004L (26093) Picosat 7 2000-004M (26094) Picosat 8 2001-043B (26930) Picosat 9 See also DRAGONSat CubeSat Los Angeles AFB References ^ a b NASA: Master Catalog of satellites ^ Stanford University: Opal Launch Vehicle ^ NASA:Master Catalog 2000-004H ^ a b PicoSat Home Page ^ Standford University: OPAL QuckFacts ^ NASA: PicoSAT 9 Mainpage ^ NASA: SpaceWarn Bulletin 556 Further reading Los Angeles AFB: DoD Experiments on Picsats Launched from STS-126 EOportal: PICOSat (STP P97-1) in-depth project review External links DoD experiments launch aboard Space Shuttle Discovery