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Project Space Track

Project Space Track was a research and development project of the US Air Force, to create a tracking system for all artificial satellites of the Earth and space probes, domestic and foreign.

Establishment
On 29 November 1957, shortly after the launch of Sputnik I on 4 October, two German expatriates, Dr. G. R. Miczaika (from Prussia) and Dr. Eberhart W. Wahl (from Berlin) formed Project Space Track (originally called Project Harvest Moon). It was established in Building 1535 of the Geophysics Research Directorate (GRD), Air Force Cambridge Research Center, Laurence G. Hanscom Field, Massachusetts. Both scientists had backgrounds in astronomy, although Dr. Wahl's PhD was in meteorology. The mission of Space Track was to create a tracking system to track and compute orbits for all artificial satellites of the Earth, including both US and Soviet payloads, booster rockets, and debris. With the Soviet launch of Luna 1 on 2 January 1959, Space Track also started tracking space probes. The first major tracking effort was Sputnik II, which was launched on 3 November 1957 and contained the dog Laika. An Electronic Support System Program Office, 496L, had been established in February 1959, with the program office at Waltham, Massachusetts under the direction of Col Victor A. Cherbak, Jr. By late 1959, the SPO had received additional responsibilities under the DoD Advanced Research Projects Agency (ARPA) to develop techniques and equipment for military surveillance of satellites Continuing development of Space Track was an integral part of this effort. Since December 1958, Space Track had been the interim National Space Surveillance Control Center. The NSSCC was part of the Air Force Command and Control Development Division (known informally as C²D²), Air Research and Development Command. Dr. Harold O. Curtis of Lincoln Laboratory was the Director of the NSSCC. The name Space Track continued in use. By 1960, there were about 70 people in the NSSCC involved in operations. Space Track continued tracking satellites and space probes until 1961. In late 1960, USAF Vice Chief of Staff General Curtis E. LeMay decided that the research and development system was ready to become operational. Eleven officers and one Senior Master Sergeant were selected to be the initial cadre of what became the 1st Aerospace Surveillance and Control Squadron. The initial cadre came to Space Track for training that started 7 November 1960. (The cadre was assigned to the new squadron on 6 March 1961.) On 1 July 1961, the new squadron became operational under the USAF Air Defense Command at Ent AFB, Colorado Springs, part of NORAD's Space Detection and Tracking System (SPADATS). The first Squadron Commander was Colonel Robert Miller. The Space Track organization at Hanscom Field assumed a backup role for squadron operations. In cavalier disregard of the Air Force Regulation on the subject, which specified clearly that unclassified nicknames, such as Space Track, should be two words (while codewords, such as [http://www.nro.gov/ CORONA, which were then themselves classified, should be only one word), ADC immediately decided to rename Space Track as SPACETRACK and the name has stuck since – although the web site of the 614th Air & Space Operations Center, which currently performs the mission, has returned to two words. The 614th is part of the Joint Space Operations Center at Vandenberg AFB, California. ==Sensors==
Sensors
. The Department of Defense had decided that the US Air Force should develop a command and control system for tracking satellites and that the US Army and US Navy should develop sensors for the purpose. US Navy development was at Dahlgren, Virginia and the US Army's program was at the Aberdeen Proving Ground, Maryland. Drs. Miczaika and Wahl had assembled a list of facilities that could track satellites, either by monitoring telemetry or by using radar. The latter were mostly astronomical radio telescopes equipped with radars used in studying the moon (e.g., Jodrell Bank Observatory in England directed by Sir Bernard Lovell, Millstone Hill of Lincoln Laboratory in Massachusetts directed by Dr. Gordon Pettingill, and a radar at the Stanford Research Institute in California, directed by Walter Jaye). Two USAF radars, one on Shemya Island in the Aleutians and the other at Diyarbakır, Turkey, had been built to observe Soviet missile launches and became valuable for satellite tracking as well. BMEWS prototype radars on Trinidad also participated. Normally, the first radar reports of a new satellite launch from Tyuratam (Baikonur) came from Shemya and the first of a new launch from Kapustin Yar came from Diyarbakır. A USAF radar at the Laredo Test Site in Texas and one at Moorestown, New Jersey also participated later. Observations were received from the Royal Canadian Air Force research radar at Prince Albert, Saskatchewan, Canada. The Goldstone facility of the Jet Propulsion Laboratory was exceptionally helpful with radio observations of Soviet space probes. In general, observations were in the form of time, azimuth and elevation (and range, from radars) as measured at the site or, in some cases, such as at Goldstone, in astronomical form (Right Ascension and Declination) Some early observations were very primitive, such as a report that a satellite passed near a star that could be identified. On rare occasions, the observations were purely verbal. For example, individuals on ships, planes, and islands in the Caribbean reported sightings of the decay of satellite 1957 β, Space track maintained close contact with the US National Security Agency, the CIA Foreign Missile and Space Analysis Center (FMSAC), and Headquarters USAF Intelligence, Major Harry Holeman. It was helpful that the USSR press service, TASS, always announced new Soviet satellite or space probe launches promptly, so Space Track was free to discuss the new objects without worrying about compromising sources. Translations of the Russian announcements were provided by the Foreign Broadcast Information Service (FBIS). ==Orbital computations==
Orbital computations
Dr. Wahl had been computing all the satellite ephemerides by hand using a Friden Square Root Calculator, the most advanced mechanical calculator then available. The method for computing ephemerides (documented in detail in a 1960 report by P.M. Fitzpatrick and G.B. Findley In October 1960, George Westrum presented a short college-level course in Celestial Mechanics for those NSSCC personnel who wished to participate ==Operations==
Operations
By international agreement under the International Astronomical Union, the satellites and space probes were initially named with Greek letters, following the system for naming stars in constellations. The year of launch was included in the launch names, so Sputnik I was 1957 Alpha. The payload was called Alpha I, when known – in the case of Sputnik I, it wasn't clear initially which was the payload, so the payload became Alpha II. Other pieces were also numbered, so the carrier rocket was usually Alpha II. The 24 Greek letters were soon used, so the next sequence started Alpha Alpha and so forth. By 1962 Beta Psi had been launched and it was clear that the Greek alphabet system would no longer work. Thereafter, launches were numbered, starting with 1963-1 with the payload normally being 1963-1A, etc... As soon as a new satellite or space probe was launched, Space Track alerted the primary sensors and processed observations as they came in, issuing a preliminary tracking bulletin promptly and updating it after about 24 hours when additional observations from around the world had been obtained. Routine bulletins continued to be issued regularly as needed to keep up with the changing orbits, some of which decayed fairly rapidly in the atmosphere. There was another flurry of activity when the last revolutions occurred, as it was difficult to forecast the exact reentry path. The NSSCC had a room dedicated as a filter center for monitoring communications and obtaining observations. The filter center had displays listing the orbiting and decayed satellites and a projector system that could show the motion of one satellite over the earth. The displays were devised by A/3C Peter P. Kamrowski. The center was staffed by a Duty Controller and assistants. The center was designed by Senior Controller 1st Lt Cotter, based on his earlier experience as a volunteer member of the USAF Ground Observer Corps (the Ground Observer Corps filter centers were in turn based on the United Kingdom aircraft tracking centers developed during World War II to track Nazi aircraft). By 1960, the position of Duty Analyst was established. Once observations had been reduced, the duty analyst reviewed them and decided which orbits needed to be recomputed to bring them up to date. In the case of new launches or decaying satellites, one analyst was dedicated to processing observations for that satellite. At this period, the 6594th Aerospace Test Wing was trying to achieve a successful launch in the Discoverer satellite program. The satellites, launched from Vandenberg AFB, were all in polar orbits. They were controlled by the 6594th at Palo Alto (later the Air Force Satellite Control Facility at Sunnyvale CA). Lt Cotter was the liaison officer between Space Track and the 6594th. The first 12 launch attempts were failures; the first success was Discoverer 1 (1959 Beta). Lockheed Corporation, the development contractor, won their bonus payment because the telemetry showed the satellite achieved orbit, but it was never seen again, despite massive Space Track and other efforts to find it. By this time Space Track had contacts with many sensors around the world. One of them was at the South Pole, associated with the International Geophysical Year. One of their ninety observations of Discoverer 2 (1959 Gamma) was sent from Byrd Station saying that the satellite had passed to the left of the zenith at 2.25 degrees, implying an orbital inclination of 89.9 degrees. This report is probably the only direct observation of the inclination of a satellite's orbit that has ever been made. Because the Discoverer satellites carried payloads that were deorbited and recovered from parachutes by aircraft of the 6594th Aerospace Test Wing based in Hawaii, the timing of deorbit was critical. (The deorbit attempt of Discoverer 2's payload went seriously wrong: the payload landed on Spitsbergen, instead of coming down over the Pacific ocean. It was recovered by Russian miners, likely very helpful to Russian intelligence and the Russian space program in general). Later, to improve the accuracy of the deorbit commands, orbital analysts Lt Algimantas Šimoliūnas, Lawrence Cuthbert, or Ed Casey would update the Space Track ephemeris for each Discoverer at the last minute and send the update to the 6594th. The 6594th had a global network of tracking stations (including Alaska, Hawaii, Seychelles, Guam, and the UK), used for command and on-orbit control of the satellites. However, the tracking data was derived from telemetry monitoring and was not as precise as the Space Track data, which was based in major part on radar and optical tracking. Lockheed decided to put a small light on Discoverer XI (1960 Delta). Space Track acted as liaison between the 6594th and the Smithsonian Astrophysical Observatory, to use their Baker-Nunn camera at Cadiz, Spain, to photograph the light. This would give Lockheed valuable information about the accuracy of their orbit computations. The experiment worked very well and was not repeated. Orbital Analysts at 1st Aero were also heavily involved in the achievement. Observations from the SPASUR fence were very helpful in tracking the fragments (SPASUR had initially refused to send Space Track individual observations, sending instead only orbital parameters, but this policy had fortunately been changed by 1961). The technique used to identify multiple objects orbiting in the same orbital plane was refined by Lawrence Cuthbert and published as an automated program by the Wolf Corporation [Later, Larry worked with Bob Morris, Chief Orbital Analyst at Colorado Springs, to develop a program to derive orbital elements for all unknown radar tracks; the methodology worked and it became known as the Cuthbert-Morris Algorithm. The resulting program was called "Breakup, Lost and Decay" and, along with subsequent improvements, it has found thousands of the objects in the Space Satellite Catalog. It is still the Air Force Astrodynamic Standard for Uncorrelated Target (UCT) processing. ==Communications==
Communications
Most Space Track communication was by teletypewriter or, in some cases, by telephone, mail, or messenger. Dr. Curtis and Lt Cotter made a similar presentation in 1960. Contractors In 1960, Aeronutronic, a division, of the Ford Motor Company, had a contract with Space Track to develop improved methods of predicting the orbits of decaying satellites, a computer program called Spiral Decay, and for other software for new computers in the new building. (Aeronutronic had been hired to do a system analysis of the control center on 1 October 1959.) Another very important group was the employees of Wolf R&D Corporation (Concord, Massachusetts), which did programming and had the contract for operating computers at the NSSCC, including the IBM 7090 mainframe. ==Further reading==
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