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 (super high frequency) band (7 to 8 GHz) to service hundreds of users.
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 1st, 2nd, and 4th satellites in the LES series were designated "X-Band satellites," designed to conduct experiments in the "X-band", the military's SHF (super high frequency) band (7 to 8 GHz)[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
LES-1, launched 11 February 1965, failed to depart from its original circular medium orbit when its onboard thruster failed to fire. The resultant tumbling and the improper orbit rendered the satellite useless for experimentation purposes.[2]: 83 [3]: 161 LES-2, launched 6 May 1965[4] was used in a number of communications experiments and met all expected objectives.[3]: 9–3 The satellite was automatically shut down by its internal clock in 1967.[3]: 9–4
With medium orbit experiments complete, the experimenters then focused on conducting X-band experiments from geosynchronous orbit[2]: 83
Spacecraft design
LES-4 was an evolution of the LES-1/2 design for a much higher orbit. It carried more solar cells[2]: 83 to run a more powerful transmitter[3]: 9–12 and a greater number of Sun and Earth sensors.[2]: 83 In addition, LES-4 was equipped with an electron spectrometer[1] to measure radiation in orbit in the 130 KeV to 4 MeV range,: 9–12 both for scientific purposes and to correlate the effect of radiation from the intense Van Allen Belts on spacecraft functions.[2]: 83 The satellite was spin stabilized, designed to rotate perpendicular to its orbital plane.[3]: 9–12
Mission and results
Titan 3C launch 22 Dec 1965
LES-4, along with LES-3, OV2-3, and OSCAR 4 was launched on the third Titan IIIC test flight[5] on 22 December 1965 at 14:00:01 UT from Cape Canaveral LC41[4] 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,[5] never occurred due to a leaking valve in the booster's attitude control system.[6]: 417 : 422 LES-3, LES-4, and OSCAR 4 were released from the Transtage, albeit much later than intended;[5] OV2-3 remained attached and did not operate.[6]: 422
Stranded in an unintended orbit, and misaligned with the sun, the satellite's solar panels only produced enough power to run onboard telemetry. Before the New Year, however, the spin axis of the satellite had precessed enough for the panels to provide sufficient power for all systems. Due to the improper orbit, the magnetic spin axis orientation system, as well as one of the onboard antenna switching control systems were rendered inoperable. The other antenna switching control system did operate properly, and all communications and scientific objectives were met.[3]: 9–2, 9–5
LES-4 stopped transmitting in October 1968.[3]: 9–4 The satellite reentered the Earth's atmosphere on 1 August 1977.[7]
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
References
^ abc"LES-4". NASA Space Science Data Coordinated Archive. Retrieved November 28, 2020.
^ abPowell, Joel W.; Richards, G.R. (1987). "The Orbiting Vehicle Series of Satellites". Journal of the British Interplanetary Society. Vol. 40. London: British Interplanetary Society.
^McDowell, Jonathan. "Satellite Catalog". Jonathon's Space Report. Retrieved February 11, 2020.
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).
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