Initial Defense Communications Satellite Program

Set of IDCSP satellites in truss of Titan IIIC Transtage
Manufacturer	TRW
Country of origin	United States
Operator	Defense Communications Agency
Applications	Satellite Communications
Specifications
Spacecraft type	Small satellite
Launch mass	45 kilograms (99 lb)
Equipment	SHF 7–8GHztransponder
Regime	Subsynchronous
Design life	6 years
Production
Status	Retired
Launched	35 (8 launch failures, 27 in orbit)
Maiden launch	16 June 1966
Last launch	13 June 1968

TheInitial Defense Communications Satellite Program orIDCSP was the firstUnited States Department of Defensecommunications satellite constellation and the first stage of theDefense Communications Satellite Program (DCSP). Launched in five groups byTitan IIIC launch vehicles to near equatorial,subsynchronous orbits between 1966 and 1968, they were intended to be experimental testbeds. They were so successful that, by the time of the launch of the last set of eight satellites, the IDCSP was deemed operational and renamedInitial Defense Satellite Communications System orIDSCS. This system allowed real-time collection of battlefield intelligence during theVietnam War. A total of 35 IDCSP satellites were launched, 27 successfully.

TheInitial Defense Communications Satellite Program orIDCSP was the first stage in theDefense Communications Satellite Program (DCSP) commissioned byUnited States Secretary of DefenseRobert McNamara in 1962. Under the DCSP, several increasingly sophisticated satellite series would test and provide long-range communications between "fixed, transportable or shipboard terminals". Development of these series would be managed by theDefense Communications Agency (DCA).^[1] This decision came on the heels of the cancellation of Project ADVENT, the first attempt at a military geosynchronous communications satellite system, begun February 1960. Originally costed at $140 million to develop, $170 million had been spent by 1962, and the estimated total cost had reached $325 million. The cheaper, "interim" IDCSP was chosen to replace ADVENT. It would use a constellation of 24-30 satellites launched intoMedium Earth Orbit via tenAtlas Agena rockets for a total cost of $165 million ($60 million of which would be spent on satellites).^[2]

Philco's Western Development Division was originally selected by theUnited States Air Force (USAF) to build the satellites.^[3] However, by 1964, the development of the much more powerfulTitan IIIC booster made it possible for fewer IDCSP satellites to fulfill the same mission at a higher altitude.^[2] Four to eight could be launched on a singleTitan IIIC rocket into slightlysubsynchronous orbit. Once there, the satellites would be deployed one at a time over the course of three minutes from the Transtage of the Titan. The satellites would drift randomly at an average rate of 28.5° per day becoming a roughly evenly spaced belt of satellites above the Earth's equator.^[4] In this way, at least one satellite of the constellation would always be visible to anEarth station if one failed.^[5] Full coverage would be provided by at least 12 satellites.^[2]

Thus, the Titan IIIC was chosen to replace the Atlas Agena as the IDCSP launch vehicle. This change did not go unchallenged; theHouse Committee on Government Operations denounced the move, saying that the "plan for short-range economies depending on a high-risk program may prove costly in the end". With the selection of the Titan IIIC as the IDCSP booster, the Pentagon dropped contract negotiations with Philco, preferring to develop the satellites in-house.^[2] Through early 1965 the satellites were still being designed so that they could be lofted to Medium Earth Orbit via Atlas Agena in the event that the Titan IIIC was not available.^[3]

The Titan IIIC was developed in time for use, the first launch taking place just four months behind the original schedule. The satellites built by 1966, sufficient for three launches, had cost just $33 million to produce (an overage of $3 million on original estimates).^[2]

Developed primarily byTRW, the IDCSP spacecraft were identicalcommunications satellites, spin-stabilized, 26-sided polygons, 86 cm (34 in) in diameter, covered with solar panels, and had a mass of 45 kilograms (99 lb).^[5] They were specifically designed to be simple to avoid the problems faced by the earlierCourier and Advent programs:^[6] no in-orbit control mechanisms were included, nor were the satellites equipped with batteries. The satellites were equipped with an automatic radiation shut-off device to deactivate them after six years in orbit.^[1]

Each satellite contained a single 3.5Watt^[7] X-band orSHFtransponder receiving at 8.025GHz and transmitting 7.25–7.3 GHz^[3] (similar to theLincoln Experimental Satellites procured around the same time)^[6] capable of concurrently supporting 600 voice or 6000teletype conversations.^[4] Complementing these satellites were ground communications terminals used to transmit and receive via IDCSP satellite voice, imagery, computerized digital data, and teletype channel usingFrequency-division multiplexing/Frequency Modulation (FDM/FM), DifferentialPhase Shift Keying (DPSK),Multiple frequency-shift keying (MFSK), andSpread Spectrum Multiple Access (SSMA) modulation techniques.^[8] TheEimac Division ofVarian Associates supplied one of the two traveling wave amplifiers used by the satellite's transmitter, the other being produced byWatkins-Johnson Company.^[2] Because of the low power of the satellites' transponders, as well as its low-gain antenna, the receiving installations had to be very large.^[7]

The first launch of IDCSP satellites took place at 14:00:01GMT on 16 June 1966 fromCape Canaveral Space Launch Complex 41 aboard the fourth Titan IIIC. After a successful Transtage burn placed the last stage of the Titan into a 33,670 km (20,920 mi) by 33,892 km (21,060 mi) orbit, the first seven IDCSP satellites (along with theGravity Gradient Technology Satellite, a stabilization test satellite built on the samesatellite bus) were dispersed one-by-one into orbit, each drifting 27.8° per day. Communications were conducted successfully betweenFort Dix, New Jersey, and sites in California, England and Germany.^[4]

The second set of IDCSP satellites, totaling eight, was lost 26 August 1966 when a faultypayload fairing caused the launch failure of the fifth Titan IIIC.^[4] This proved to be the last unsuccessful Titan IIIC launch.^[4]

On 18 January 1967, the seventh Titan IIIC launch successfully placed a full constellation of eight IDCSP satellites into orbit,^[4] and on 1 July 1967, four more IDCSP satellites (including IDCSP 19, also known as DATS (Despun Antenna Test Satellite)) were put into orbit.^[9] IDCSP ground terminals had been installed at American bases atSaigon andNha Trang by that time. Despite the comparative simplicity of the IDCSP constellation satellites, under Project Compass Link, the satellites made it possible for high-resolution photography to be transferred between theSouth Vietnamese capital andWashington, D.C., allowing near-real-time battlefield analysis.^[6] With the launch of the fourth system of eight satellites on 13 June 1968, DCA deemed the experimental system operational, renaming it the Initial Defense Satellite Communications System (IDSCS). This system afforded the American military a secure system for sensitive command-and-control communications, the more routine administrative and logistical messages being relayed via commercial satellites.^[6] The IDCSP constellation was also used byNorth Atlantic Treaty Organization states, which referred to the program as NATO-1.^[9]

In all, 35 IDCSP satellites were launched in 5 groups by Titan IIIC launch vehicles, 27 successfully^[10] to near equatorial,subsynchronous orbits. The automatic shut-off device installed on the IDCSP satellites did not work reliably, and many satellites operated long past their six-year lifespan. As of 1975, six were still functioning.^[1]

Technical and systems management assistance was provided to the USAF'sSpace Systems Division byThe Aerospace Corporation.^[2] The IDCSP series was succeeded by the NATO-2 and DSCS-2 truegeosynchronous satellites.^[5]

• 1966 in spaceflight
• 1967 in spaceflight
• 1968 in spaceflight
• Communications satellite constellations
• Military communications
• Military space program of the United States
• Satellite series
• Spacecraft launched by Titan rockets
• Military equipment introduced in the 1960s

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