LES-3

Last updated

LES-3
LES-3 satellite drawing.jpg
Mission type Communications satellite
Operator USAF
COSPAR ID 1965-108D OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 01941 OOjs UI icon edit-ltr-progressive.svg
Spacecraft properties
Manufacturer Lincoln Laboratory
Launch mass16 kg (35 lb) [1]
Start of mission
Launch date21 December 1965, 14:00:01 (1965-12-21UTC14:00:01)
Rocket Titan IIIC
Launch site Cape Canaveral LC41
End of mission
Last contactLate summer 1967
Decay date6 April 1968
Orbital parameters
Reference system Geocentric
Regime Highly elliptical
Eccentricity 0.71486
Perigee altitude 195 km (121 mi)
Apogee altitude 33,177.00 km (20,615.23 mi)
Inclination 26.4°
Period 581.80 minutes [1]
Epoch 21 December 1965 15:36:00
LES
  LES-2
LES-4  
 

Lincoln Experimental Satellite 3, also known as LES-3, was a communications satellite, the third of nine in the Lincoln Experimental Satellite. Launched by the United States Air Force (USAF) on 21 Dec 1965, it was stranded in a Geostationary Transfer Orbit rather than its planned circular high orbit. Despite this, LES-3 returned good data on communications propagation in the UHF band.

Contents

Background

After the successful development and deployment of Project West Ford, a passive communications system consisting of orbiting copper needles, MIT's Lincoln Laboratory turned to improving active-satellite space communications. In particular, Lincoln aimed to increase the transmission capability of communications satellites ("downlink"), which was necessarily constrained by their limited size. After receiving a charter in 1963 to build and demonstrate military space communications, Lincoln focused on a number of engineering solutions to the downlink problem including improved antennas, better stabilization of satellites in orbit (which would benefit both downlink and "uplink"—communications from the ground), high-efficiency systems of transmission modulation/de-modulation, and cutting-edge error-checking techniques. [2] :81–83

These experimental solutions were deployed in a series of nine spacecraft called Lincoln Experimental Satellites (LES). Concurrent with their development, Lincoln also developed the Lincoln Experimental Terminals (LET), ground stations that used interference-resistant signaling techniques that allowed use of communications satellites by up to hundreds of users at a time, mobile or stationary, without involving elaborate systems for synchronization and centralized control. [2] :81–83

The first experimental solution, demonstrated by LES-1, LES-2, and LES-4, involved communications in the "X-band", the military's SHF (super high frequency) band (225 to 400 MHz) [3] :9–1 because solid-state equipment allowed for comparatively high output in this band, and also because the band had been previously used by West Ford. [2] :83–84

The SHF band was not usable for small, tactical deployment as it required large terminals and ground antennas. Lincoln Laboratories thus also explored using the UHF band for communications. After an initial survey program, in which aircraft were flown over cities and varied landscapes to measure ambient radio noise, LES-3 was developed specifically to explore propagation phenomena between satellites and airborne terminals. Because the Earth's surface was mirror-smooth relative to the one-meter wavelength of median UHF frequencies, transmissions could be sent from satellite to airborne terminals by multiple paths. By determining the likely parameters of signal delays, Lincoln engineers could create robust systems that accommodated for multipath propagation effects. [2] :84

Spacecraft design

LES-3 was produced quickly using technology from the three LES X-band satellites (-1, -2, and -4). Its primary function was simply to broadcast continuously [2] at a frequency of 232.9 MHz. [3] :9–27

Polyhedral in shape, and 5 ft (1.5 m) across, the solar powered [4] satellite utilized the frame, power system, and power amplifiers designed for LES-1 and 2 and was similar in appearance to its predecessors. [3] :9–31 It differed in its omission of optical sensors, and the substitution of a UHF monopole antenna projecting from the top and bottom of the satellite's rectangular top and bottom for LES-1/2's X-band antennas. As a result, LES-3 massed just 16 kilograms (35 lb), [1] about half of its predecessors. [5] [6]

The satellite was spin stabilized. [3] :9–31

Mission and results

Titan 3C launch 22 Dec 1965 Titan3C launch 22 Dec 1965.jpg
Titan 3C launch 22 Dec 1965

LES-3, along with LES-4, OV2-3, and OSCAR 4 was launched on the third Titan IIIC test flight [7] on 22 December 1965 at 14:00:01 UT from Cape Canaveral LC41 [8] just one second behind schedule. From an initial parking orbit of 194 kilometres (121 mi), the Titan's Transtage boosted into a transfer orbit pending a final burn to circularize its orbit. However, this final burn, scheduled for T+6:03:04 after liftoff, [7] never occurred due to a leaking valve in the booster's attitude control system. [9] :417:422 LES-3, LES-4, and OSCAR 4 were released from the Transtage, albeit much later than intended; [7] OV2-3 remained attached and did not operate. [9] :422

Despite being placed in an unexpected orbit, spinning at 140 RPM inclined about 15° to the orbital plane (as opposed to perpendicularly, as had been planned), LES-3 functioned properly, providing signals necessary for UHF propagation measurements. [3] :9–20

The satellite reentered on 6 April 1968, [10] earlier than planned, but not before all desired testing had been successfully completed [3] :9–20 in late summer 1967. [3] :9–21

Legacy and status

The LES program continued through nine satellites, culminating in the launch of LES-8 and LES-9 on 14 March 1976. [2] :88

Related Research Articles

<span class="mw-page-title-main">Communications satellite</span> Artificial satellite that relays radio signals

A communications satellite is an artificial satellite that relays and amplifies radio telecommunication signals via a transponder; it creates a communication channel between a source transmitter and a receiver at different locations on Earth. Communications satellites are used for television, telephone, radio, internet, and military applications. Many communications satellites are in geostationary orbit 22,300 miles (35,900 km) above the equator, so that the satellite appears stationary at the same point in the sky; therefore the satellite dish antennas of ground stations can be aimed permanently at that spot and do not have to move to track the satellite. Others form satellite constellations in low Earth orbit, where antennas on the ground have to follow the position of the satellites and switch between satellites frequently.

<span class="mw-page-title-main">Ultra high frequency</span> Electromagnetic spectrum 300–3000 MHz

Ultra high frequency (UHF) is the ITU designation for radio frequencies in the range between 300 megahertz (MHz) and 3 gigahertz (GHz), also known as the decimetre band as the wavelengths range from one meter to one tenth of a meter. Radio waves with frequencies above the UHF band fall into the super-high frequency (SHF) or microwave frequency range. Lower frequency signals fall into the VHF or lower bands. UHF radio waves propagate mainly by line of sight; they are blocked by hills and large buildings although the transmission through building walls is strong enough for indoor reception. They are used for television broadcasting, cell phones, satellite communication including GPS, personal radio services including Wi-Fi and Bluetooth, walkie-talkies, cordless phones, satellite phones, and numerous other applications.

<span class="mw-page-title-main">Skynet (satellite)</span> Communications satellite

Skynet is a family of military communications satellites, now operated by Airbus Defence and Space on behalf of the United Kingdom's Ministry of Defence (MoD). They provide strategic and tactical communication services to the branches of the British Armed Forces, the British intelligence agencies, some UK government departments and agencies, and to allied governments. Since 2015 when Skynet coverage was extended eastward, and in conjunction with an Anik G1 satellite module over America, Skynet offers near global coverage.

<span class="mw-page-title-main">Titan IIIC</span> Expendable launch system used by the US Air Force

The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly. The majority of the launcher's payloads were DoD satellites, for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB.

<span class="mw-page-title-main">Milstar</span> Constellation of American military satellites

Milstar is a constellation of military communications satellites in geosynchronous orbit, which are operated by the United States Space Force, and provide secure and jam-resistant worldwide communications to meet the requirements of the Armed Forces of the United States. Six spacecraft were launched between 1994 and 2003, of which only five were operational after launch; the third launch failed, both damaging the satellite and leaving it in an unusable orbit.

<span class="mw-page-title-main">ATS-6</span> NASA experimental satellite

ATS-6 was a NASA experimental satellite, built by Fairchild Space and Electronics Division It has been called the world's first educational satellite as well as world's first experimental Direct Broadcast Satellite as part of the Satellite Instructional Television Experiment between NASA and Indian Space Research Organisation (ISRO). It was launched May 30, 1974, and decommissioned July 1979. At the time of launch, it was the most powerful telecommunication satellite in orbit. ATS-6 carried no fewer than 23 different experiments, and introduced several breakthroughs. It was the first 3-axis stabilized spacecraft in geostationary orbit. It was also the first to use experimentally with some success electric propulsion in geostationary orbit. It also carried several particle physics experiments, including the first heavy ion detector in geostationary orbit.

<span class="mw-page-title-main">Fleet Satellite Communications System</span>

FLTSATCOM is a satellite communication system controlled by the U.S. Space Force which was used for UHF radio communications between ships, submarines, airplanes and ground stations of the Navy.

<span class="mw-page-title-main">Advanced Extremely High Frequency</span> Series of American military satellites

Advanced Extremely High Frequency (AEHF) is a constellation of communications satellites operated by the United States Space Force. They are used to relay secure communications for the United States Armed Forces, the British Armed Forces, the Canadian Armed Forces, the Netherlands Armed Forces and the Australian Defence Force. The system consists of six satellites in geostationary orbits. The final satellite was launched on 26 March 2020. AEHF is backward compatible with, and replaces, the older Milstar system and will operate at 44 GHz uplink and 20 GHz downlink. The AEHF system is a joint service communications system that provides survivable, global, secure, protected, and jam-resistant communications for high-priority military ground, sea and air assets.

<span class="mw-page-title-main">Lincoln Experimental Satellite</span> Experimental Satellite series for testing devices and techniques for satellite communication

The Lincoln Experimental Satellite series was designed and built by Lincoln Laboratory at Massachusetts Institute of Technology between 1965 and 1976, under USAF sponsorship, for testing devices and techniques for satellite communication.

This is an index to articles about terms used in discussion of radio propagation.

<span class="mw-page-title-main">Unified S-band</span>

The Unified S-band (USB) system is a tracking and communication system developed for the Apollo program by NASA and the Jet Propulsion Laboratory (JPL). It operated in the S band portion of the microwave spectrum, unifying voice communications, television, telemetry, command, tracking and ranging into a single system to save size and weight and simplify operations. The USB ground network was managed by the Goddard Space Flight Center (GSFC). Commercial contractors included Collins Radio, Blaw-Knox, Motorola and Energy Systems.

<span class="mw-page-title-main">OSCAR 4</span> Amateur radio satellite

OSCAR IV was the fourth amateur radio satellite launched by Project OSCAR and the first targeted for Geostationary orbit on 12 December 1965. The satellite was launched piggyback with three United States Air Force satellites on a Titan IIIC launch vehicle. Due to a booster failure, OSCAR 4 was placed in an unplanned and largely unusable Geostationary transfer orbit.

<span class="mw-page-title-main">Mars Cube One</span> 2018 Mars flyby mission

Mars Cube One was a Mars flyby mission launched on 5 May 2018 alongside NASA's InSight Mars lander. It consisted of two nanospacecraft, MarCO-A and MarCO-B, that provided real-time communications to Earth for InSight during its entry, descent, and landing (EDL) on 26 November 2018 - when InSight was out of line of sight from the Earth. Both spacecraft were 6U CubeSats designed to test miniaturized communications and navigation technologies. These were the first CubeSats to operate beyond Earth orbit, and aside from telecommunications they also tested CubeSats' endurance in deep space. On 5 February 2019, NASA reported that both the CubeSats had gone silent by 5 January 2019, and are unlikely to be heard from again. In August 2019, the CubeSats were honored for their role in the successful landing of the InSight lander on Mars.

<span class="mw-page-title-main">OV2-1</span> US Air Force satellite

Orbiting Vehicle 2-1, the first satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American life science research satellite. Its purpose was to determine the extent of the threat posed to astronauts by the Van Allen radiation belts. Launched 15 October 1965, the mission resulted in failure when the upper stage of OV2-1's Titan IIIC booster broke up.

<span class="mw-page-title-main">LES-1</span> Former communications satellite

Lincoln Experimental Satellite 1, also known as LES-1, was a communications satellite, the first of nine in the Lincoln Experimental Satellite program. Launched by the United States Air Force (USAF) on February 11, 1965, it pioneered many then-advanced technologies including active use of the military's SHF band to service hundreds of users. LES-1 did not have a successful operational life due to being placed in a suboptimal orbit, and it ceased transmissions in 1967. After 45 years of inactivity, LES-1 spontaneously resumed transmissions in 2012 making it one of the oldest zombie satellites.

<span class="mw-page-title-main">LES-2</span> Former communications satellite

Lincoln Experimental Satellite 2, also known as LES-2, was a communications satellite, the second of nine in the Lincoln Experimental Satellite. Launched by the United States Air Force (USAF) on 6 May 1965, it demonstrated many then-advanced technologies including active use of the military's SHF band to service hundreds of users.

<span class="mw-page-title-main">OV2-3</span> US Air Force satellite

Orbiting Vehicle 2-3, the second satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American solar astronomy, geomagnetic and particle science research satellite. Launched 22 December 1965 along with three other satellites, the mission resulted in failure when the spacecraft failed to separate from the upper stage of its Titan IIIC.

<span class="mw-page-title-main">LES-4</span> Former communications satellite

Lincoln Experimental Satellite 4, also known as LES-4, was a communications satellite, the fourth of nine in the Lincoln Experimental Satellite, and the first of the series designed for operations at geosynchronous altitudes. Launched by the United States Air Force (USAF) on 21 December 1965, it demonstrated many then-advanced technologies including active use of the military's SHF band to service hundreds of users.

<span class="mw-page-title-main">Initial Defense Communications Satellite Program</span> American satellite family

The Initial Defense Communications Satellite Program or IDCSP was the first United States Department of Defense communications satellite constellation and the first stage of the Defense Communications Satellite Program (DCSP). Launched in five groups by Titan 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 renamed Initial Defense Satellite Communications System or IDSCS. This system allowed real-time collection of battlefield intelligence during the Vietnam War. A total of 35 IDCSP satellites were launched, 27 successfully.

<span class="mw-page-title-main">OV2-5</span> US Air Force satellite

Orbiting Vehicle 2-5, the third and last satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American particle science and ionosphere research satellite. Launched 26 September 1968 along with three other satellites, OV2-5 became the first scientific satellite to operate at geosynchronous altitude.

References

  1. 1 2 3 "LES-3". NASA Space Science Data Coordinated Archive. Retrieved November 27, 2020.
  2. 1 2 3 4 5 6 Andrew J. Butrica, ed. (1997). Beyond the Ionosphere: Fifty Years of Satellite Communication (PDF). Washington D.C.: NASA History Office. Retrieved May 30, 2023.
  3. 1 2 3 4 5 6 7 NASA COMPENDIUM OF SATELLITE COMMUNICATIONS PROGRAMS (PDF). Greenbelt, MD: Goddard Spaceflight Center. 1973.
  4. "Third Titan 3A Vehicle Carries Experimental Comsat into Orbit" . Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. February 16, 1965. Retrieved February 16, 2020.
  5. "LES-1". NASA Space Science Data Coordinated Archive. Retrieved February 17, 2020.
  6. "LES-2". NASA Space Science Data Coordinated Archive. Retrieved May 2, 2020.
  7. 1 2 3 "Titan 3 Transtage Malfunctions, Fails to Achieve Circular Orbit" . Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. December 27, 1965. p. 27. Retrieved November 24, 2020.
  8. McDowell, Jonathan. "Launch Log". Jonathon's Space Report. Retrieved December 30, 2018.
  9. 1 2 Powell, Joel W.; Richards, G.R. (1987). "The Orbiting Vehicle Series of Satellites". Journal of the British Interplanetary Society. Vol. 40. London: British Interplanetary Society.
  10. McDowell, Jonathan. "Satellite Catalog". Jonathon's Space Report. Retrieved February 11, 2020.