![]() The Atlas F used MA-5 engines on the booster and the sustainer. During the sixth orbit, a massive electrical power failure occurred aboard MIDAS 5, and all control over the vehicle was lost. Atlas E is capable of boosting a 4,000-pound payload to a 450-nmi orbit. Turned on, the infrared payload checked out during the first few orbits of the Earth. The spacecraft achieve its planned polar orbit, stabilized properly, and the solar arrays extended and began generating the needed electrical power. MIDAS 5, the third and last of the Series 2 flights carrying a Baird-Atomic infrared payload, lifted from Vandenberg AFB on 9 April 1962. Two deployable solar arrays were mounted on the aft equipment rack of the Agena-B to provide power. The increased tankage and a new dual-burn rocket engine would permit reaching a planned circular polar orbit at an altitude of 3400 km, the orbit then considered most appropriate for an operational constellation of MIDAS satellites. The Agena-B was nearly twice the length of its Agena-A predecessor. Marshall was to spend no more than 2 million, however, until a Statement of Work had been made definite. Manned Spacecraft Center (MSC) suballotted 5.2 million to Marshall Space Flight Center for procuring Atlas-Agena vehicles for Project Gemini. The Agena-B upper stage of the Atlas-LV3 Agena-B launch vehicle was used as the spacecraft bus and provided power and attitude control to the MIDAS payload. 5.2 million for Atlas-Agena vehicles for Project Gemini. MIDAS Series 2 carried a new infrared payload built by Baird-Atomic, one that featured 175 detectors capable of sensing ICBM targets at a maximum slant range of 4200 nm, The payload was designed to scan at a rate of 6 rpm, a rate of rotation three times faster than the Series I payloads. MIDAS technology was undeniably demonstrated payload performance markedly exceeded expectations in the detection of solid-propellant rockets.The MIDAS Series 2 (Military Defense Alarm System) satellites, MIDAS 3, 4, and 5, were the second development models for the MIDAS early warning system. 400-series uses standard 4.2 m diameter Atlas payload fairing, 500-series uses. ![]() The Aerojet Series III payload achieved an operating radiance level sensitivity, with signal-to-noise, of 50 kw/STR. Atlas Agena A: (1960) Also known as LV-3A. These missiles included not only three liquid propellant Atlas and Titan ICBMs but offline tapes also revealed the detection of seven lower radiance solid propellant Minuteman and Polaris missiles. In its six-week operational period, MIDAS 7 detected all of the ballistic missiles launched within its field of view. Two deployable solar arrays were mounted on the aft equipment rack of the Agena-B to provide power. Atlas General Agency is proud to serve Texas independent insurance agents and their policyholders. The Agena-B upper stage of the Atlas-LV3 Agena-B launch vehicle was used as the spacecraft bus and provided power and attitude control to the MIDAS payload. The basic spacecraft remained unchanged from the Series II, except for reliability upgrades. The 2.7-micron system provided both spectral and spatial background rejection, and emphasized boost phase detection of missiles in the "Atlas class." The telescope rotated on its spin table at 6 rpm, like its Baird-Atomic predecessor. Nr TNr Vehicle Serial Date LS Payload 179 1 Atlas-LV3 Agena-D 201D Va LC-2-3 KH-7 1 186 2 Atlas-LV3 Agena-D 212D Va LC-2-3 KH-7 2 192 3 Atlas-LV3 Agena-D 197D CC LC-13 Vela 1 / Vela 2 / ERS 12 193 4 Atlas-LV3 Agena-D. The detector array on the surface of the focal-plane assembly contained 184 lead sulfide detectors arranged in eight vertical columns of 23 detectors each which provided complete vertical coverage of a 24-degree 58-minute field of view. The fourth of these launches failed when one of the booster unit engines shut down early. citation needed Atlas E/F-MSD edit Atlas E/F rockets with MSD upper stages were used for four launches, with NOSS naval reconnaissance satellites between 19. It featured a Bouwers concentric telescope with an 8-inch aperture. The rocket had a payload capacity of 950 kg (2,090 lb) to low Earth orbit. The Series III carried an improved Aerojet-General infrared payload. The MIDAS Series 3 (Military Defense Alarm System) satellites, MIDAS 6, 7, 8, and 9, were the third development models for the MIDAS early warning system.
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