Initial Defense Communications Satellite Program

The Initial Defense Communications Satellite Program or IDCSP was the first stage in the Defense Communications Satellite Program (DCSP) commissioned by United States Secretary of Defense Robert 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 the Defense Communications Agency (DCA).{{cite book|url=https://archive.org/details/communicatingbys1094520778|title=Communicating by Satellite|author=Robert Earl Bird|date=1975|publisher=Naval Postgraduate School|location=Monterey, California|oclc=1042380582|pages=29–30}} 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 into Medium Earth Orbit via ten Atlas Agena rockets for a total cost of $165 million ($60 million of which would be spent on satellites).{{cite magazine|date=27 June 1966|title="DOD Communications Satellite Set|url=http://archive.aviationweek.com/issue/19660627#!&pid=25|magazine=Aviation Week and Space Technology|publisher=McGraw Hill Publishing Company|access-date=25 May 2021|pages=25–26|url-access=subscription}}

Philco's Western Development Division was originally selected by the United States Air Force (USAF) to build the satellites.{{cite magazine|date=9 May 1966|title="DOD Communications Satellite Set|url=http://archive.aviationweek.com/issue/19660509#!&pid=32|magazine=Aviation Week and Space Technology|publisher=McGraw Hill Publishing Company|access-date=27 April 2021|page=33|url-access=subscription}} However, by 1964, the development of the much more powerful Titan IIIC booster made it possible for fewer IDCSP satellites to fulfill the same mission at a higher altitude. Four to eight could be launched on a single Titan IIIC rocket into slightly subsynchronous 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.{{cite web|url=https://www.drewexmachina.com/2015/06/18/the-first-missions-of-the-titan-iiic/|title=The First Missions of the Titan IIIC|author=Andrew LePage|publisher=Drew Ex Machina|date=18 June 2015|access-date=28 April 2021}} In this way, at least one satellite of the constellation would always be visible to an Earth station if one failed.{{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1966-053B|title=IDCSP 1-1|publisher=NASA |access-date=27 April 2021}} {{PD-notice}} Full coverage would be provided by at least 12 satellites.

Thus, the Titan IIIC was chosen to replace the Atlas Agena as the IDCSP launch vehicle. This change did not go unchallenged; the House 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. 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.

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).

File:IDCSP 001.jpg

Developed primarily by TRW, the IDCSP spacecraft were identical communications satellites, spin-stabilized, 26-sided polygons, {{cvt|86|cm}} in diameter, covered with solar panels, and had a mass of {{convert|45|kg}}. They were specifically designed to be simple to avoid the problems faced by the earlier Courier and Advent programs:{{cite book |first1=David N. |last1=Spires |first2=Rick W. |last2=Sturdevant |contribution=From Advent to Milstar: The U.S. Air Force and the Challenges of Military Satellite Communications |title=Beyond the Ionosphere: Fifty Years of Satellite Communication|editor-first=Andrew J. |editor-last=Butica|publisher=NASA|location=Washington, D.C.|date=1997|id=SP-4217|url=https://history.nasa.gov/SP-4217/sp4217.htm|pages=68–69, 83|bibcode=1997bify.book.....B }} 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.

Each satellite contained a single 3.5 Watt{{cite web|url=https://apps.dtic.mil/sti/pdfs/ADA300320.pdf|archive-url=https://web.archive.org/web/20210514142233/https://apps.dtic.mil/sti/pdfs/ADA300320.pdf|url-status=live|archive-date=May 14, 2021|title=DSCS - Past, Present, and Future|author=Robert Cook|date=March 1994|publisher=Defense Technical Information Center|location=Alexandria, Virginia}} X-band or SHF transponder receiving at 8.025 GHz and transmitting 7.25–7.3 GHz (similar to the Lincoln Experimental Satellites procured around the same time) capable of concurrently supporting 600 voice or 6000 teletype conversations. Complementing these satellites were ground communications terminals used to transmit and receive via IDCSP satellite voice, imagery, computerized digital data, and teletype channel using Frequency-division multiplexing/Frequency Modulation (FDM/FM), Differential Phase Shift Keying (DPSK), Multiple frequency-shift keying (MFSK), and Spread Spectrum Multiple Access (SSMA) modulation techniques.{{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1966-066A|title=IDCSP 3-1|publisher=NASA |access-date=27 April 2021}} {{PD-notice}} The Eimac Division of Varian Associates supplied one of the two traveling wave amplifiers used by the satellite's transmitter, the other being produced by Watkins-Johnson Company. Because of the low power of the satellites' transponders, as well as its low-gain antenna, the receiving installations had to be very large.

File:Idcspdep.jpg

The first launch of IDCSP satellites took place at 14:00:01 GMT on 16 June 1966 from Cape Canaveral Space Launch Complex 41 aboard the fourth Titan IIIC. After a successful Transtage burn placed the last stage of the Titan into a {{cvt|33670|km}} by {{cvt|33892|km}} orbit, the first seven IDCSP satellites (along with the Gravity Gradient Technology Satellite, a stabilization test satellite built on the same satellite bus) were dispersed one-by-one into orbit, each drifting 27.8° per day. Communications were conducted successfully between Fort Dix, New Jersey, and sites in California, England and Germany.

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

On 18 January 1967, the seventh Titan IIIC launch successfully placed a full constellation of eight IDCSP satellites into orbit, and on 1 July 1967, four more IDCSP satellites (including IDCSP 19, also known as DATS (Despun Antenna Test Satellite)) were put into orbit.{{cite web|url=https://space.skyrocket.de/doc_sdat/idcsp.htm|title=IDCSP → DSCS-1 (NATO 1)|last=Krebs|first=Gunter|publisher=Gunter's Space Page|access-date=12 May 2021}} IDCSP ground terminals had been installed at American bases at Saigon and Nha 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 the South Vietnamese capital and Washington, D.C., allowing near-real-time battlefield analysis. 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. The IDCSP constellation was also used by North Atlantic Treaty Organization states, which referred to the program as NATO-1.

In all, 35 IDCSP satellites were launched in 5 groups by Titan IIIC launch vehicles, 27 successfully{{Cite web|url=https://www.planet4589.org/space/log/satcat.txt|title=Satellite Catalog|last=McDowell|first=Jonathan|publisher=Jonathon's Space Report|access-date=27 April 2021}} 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.

Technical and systems management assistance was provided to the USAF's Space Systems Division by The Aerospace Corporation. The IDCSP series was succeeded by the NATO-2 and DSCS-2 true geosynchronous satellites.

File:Titan IIIC-11 launch.jpg

File:TITAN IIIC IDCSP SATELLITE MISSION FROM PAD 41 - 18 January 1967.jpg

File:AN TSC-54 ground terminal.jpg

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{{Orbital launches in 1966}}

{{Orbital launches in 1967}}

{{Orbital launches in 1968}}

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Category:1966 in spaceflight

Category:1967 in spaceflight

Category:1968 in spaceflight

Category:Communications satellite constellations

Category:Military communications

Category:Military space program of the United States

Category:Satellite series

Category:Spacecraft launched by Titan rockets

Category:Military equipment introduced in the 1960s