Encyclopedia Astronautica
FalconSat


American technology satellite. 3 launches, 2000.01.27 (Falconsat) to 2007.03.09 (Falconsat-3). The JAWSAT/FalconSat payloads were developed as a joint effort between the Air Force Academy and Weber State University.

First Launch: 2000.01.27.
Last Launch: 2007.03.09.
Number: 3 .

More... - Chronology...


Associated Countries
See also
  • Atlas V The Atlas V launch vehicle system was a completely new design that succeeded the earlier Atlas series. Atlas V vehicles were based on the 3.8-m (12.5-ft) diameter Common Core Booster (CCB) powered by a single Russian RD-180 engine. These could be clustered together, and complemented by a Centaur upper stage, and up to five solid rocket boosters, to achieve a wide range of performance. More...
  • Falcon Falcons are a family of two stage, reusable, liquid oxygen and kerosene powered launch vehicles, designed for cost-efficient and reliable transport of satellites and manned spacecraft to low Earth orbit. The Falcon 1 satellite launcher began launches in 2006, with the Falcon 9 - as large as a Saturn I - flying in 2010. The Falcon series was the only successful project among many attempts to privately develop a low cost launch system since the 1960's. More...
  • Minotaur Minotaur was developed for the US Air Force's Orbital/Suborbital Program (OSP) as a low-cost, four-stage Space Launch Vehicle (SLV) using a combination of government-supplied surplus Minuteman II ICBM motors and proven Orbital space launch technologies. Proposed growth versions would use surplus Peacekeeper rocket stages. More...

Associated Launch Vehicles
  • Minotaur 1 American all-solid orbital launch vehicle. Orbital launch vehicle consisting of a surplus Minuteman M55A1 first stage, Minuteman SR19 second stage, and new Orion 50XL third stage, Orion 38 fourth stage, and optional HAPS fifth stage for velocity trim and multiple payload deployment. Payload 580 kg to an 185 km, 28.5 degree orbit from Cape Canaveral; 310 kg to a 740 km sun-synchronous orbit from Vandenberg. More...
  • Atlas V 401 American orbital launch vehicle. Atlas V version with a 4-m diameter payload fairing, single engine Centaur upper stage, and no strap-on solid boosters. Payloads: 7,095 kg (15,642 lb) to sun synchronous orbit; 4,950 kg (10,910 lb) to geosynchronous transfer orbit. More...
  • Falcon 1 American low cost orbital launch vehicle. Falcon I was a two stage, reusable, liquid oxygen and kerosene powered launch vehicle. A single engine powered the first stage. It was designed for cost-efficient and reliable transport of satellites to low Earth orbit. First launch of the Falcon I was scheduled for mid-2004 from Vandenberg, carrying a US Defense Department communications satellite. Development delays and problems with USAF clearances for launch from Vandenberg resulted in the first launch attempt being made in 2006 from a private facility at Omelek near Kwajalein atoll in the Pacific. Success was achieved on the fourth launch in 2008. The Falcon 1 was to be superseded by the Falcon 1e, with an extended-tank first stage, from 2010. More...

Associated Manufacturers and Agencies
  • Weber American manufacturer of spacecraft. Weber State University, Utah, USA. More...

Bibliography
  • California SpacePort Home Page, Web Address when accessed: here.

Associated Launch Sites
  • Cape Canaveral America's largest launch center, used for all manned launches. Today only six of the 40 launch complexes built here remain in use. Located at or near Cape Canaveral are the Kennedy Space Center on Merritt Island, used by NASA for Saturn V and Space Shuttle launches; Patrick AFB on Cape Canaveral itself, operated the US Department of Defense and handling most other launches; the commercial Spaceport Florida; the air-launched launch vehicle and missile Drop Zone off Mayport, Florida, located at 29.00 N 79.00 W, and an offshore submarine-launched ballistic missile launch area. All of these take advantage of the extensive down-range tracking facilities that once extended from the Cape, through the Caribbean, South Atlantic, and to South Africa and the Indian Ocean. More...
  • Vandenberg Vandenberg Air Force Base is located on the Central Coast of California about 240 km northwest of Los Angeles. It is used for launches of unmanned government and commercial satellites into polar orbit and intercontinental ballistic missile test launches toward the Kwajalein Atoll. More...
  • Kwajalein The US military base located on this Pacific island group has major tracking facilities and is near the impact area for dummy warheads fired by ICBM's from Vandenberg AFB. It is a key test location for anti-ballistic missile systems. More...
  • Cape Canaveral LC41 Titan, Atlas V launch complex. Complexes 40 and 41 were constructed as part of the Integrate-Transfer-Launch (ITL) Titan launch facility at the north end of Cape Canaveral in the early 1960s. Over the next three decades, the complexes supported a wide variety of military space missions involving Titan IIIC, Titan 34D and Titan IV. Complex 41 was deactivated at the end of 1977, then upgraded for the Titan IV program in the 1986-88 period. In October 1999, Complex 41 was demolished with high explosives in order for a new pad for launch of the Atlas 5 rocket to be erected. By then it had been the starting point for 27 Titan flights. More...

FalconSat Chronology


2000 January 27 - . 03:03 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC8. LV Family: Minotaur. Launch Vehicle: Minotaur 1. LV Configuration: Minotaur 1OSP / SLV-1.
  • Falconsat - . Mass: 52 kg (114 lb). Nation: USA. Agency: USAF AFMC. Manufacturer: USAF Colorado Springs. Class: Technology. Type: Navigation technology satellite. Spacecraft: Falconsat. USAF Sat Cat: 26064 . COSPAR: 2000-004D. Apogee: 810 km (503 mi). Perigee: 754 km (468 mi). Inclination: 100.2003 deg. Period: 100.41 min. Summary: USAF Academy satellite, carried the CHAWS-LD (Charging Hazards and Wake Studies-Long Duration) experiment to measure spacecraft charging effects in LEO..

2006 March 24 - . Launch Site: Kwajalein. Launch Complex: Kwajalein OM. LV Family: Falcon. Launch Vehicle: Falcon 1. LV Configuration: Falcon 1 1. FAILURE: Fuel leak at T+25 seconds caused a fire in the first stage engine area. Failed Stage: 1.
  • Falconsat-2 - . Mass: 20 kg (44 lb). Nation: USA. Agency: USAF Colorado Springs. Manufacturer: USAFA. Class: Technology. Type: Navigation technology satellite. Spacecraft: Falconsat. COSPAR: F20060324. Summary: The satellite fell through the roof of SpaceX's machine shop on the atoll..

2007 March 9 - . 03:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 401. LV Configuration: Atlas V 401 AV-013.
  • Falconsat-3 - . Mass: 50 kg (110 lb). Nation: USA. Agency: Martin. Manufacturer: USAF Colorado Springs. Class: Technology. Type: Navigation technology satellite. Spacecraft: Falconsat. USAF Sat Cat: 30776 . COSPAR: 2007-006E. Apogee: 559 km (347 mi). Perigee: 558 km (346 mi). Inclination: 35.4000 deg. Period: 95.80 min. Summary: USAF Academy student satellite with ionospheric experiments and plasma atttiude control thrusters..

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