Names | S-55B NASA S-55B | ||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Mission type | Micrometeoroid research | ||||||||||||
Operator | NASA | ||||||||||||
Harvard designation | 1962 Beta Chi 1 | ||||||||||||
COSPAR ID | 1962-070A | ||||||||||||
SATCAT no. | 00506 | ||||||||||||
Mission duration | 7.5 months (achieved) | ||||||||||||
Spacecraft properties | |||||||||||||
Spacecraft | Explorer XVI | ||||||||||||
Spacecraft type | Science Explorer | ||||||||||||
Bus | S-55 | ||||||||||||
Manufacturer | Goddard Space Flight Center | ||||||||||||
Launch mass | 100.8 kg (222 lb) | ||||||||||||
Dimensions | 61 × 192 cm (24 × 76 in) cylinder | ||||||||||||
Power | Solar cells and nickel-cadmium batteries | ||||||||||||
Start of mission | |||||||||||||
Launch date | 16 December 1962, 14:33:04 GMT [1] | ||||||||||||
Rocket | Scout X-3 (S-115) | ||||||||||||
Launch site | Wallops Flight Facility, LA-3 | ||||||||||||
Contractor | Vought | ||||||||||||
Entered service | 16 December 1962 | ||||||||||||
End of mission | |||||||||||||
Last contact | Late July 1963 | ||||||||||||
Orbital parameters | |||||||||||||
Reference system | Geocentric orbit [2] | ||||||||||||
Regime | Low Earth orbit | ||||||||||||
Perigee altitude | 750 km (470 mi) | ||||||||||||
Apogee altitude | 1,181 km (734 mi) | ||||||||||||
Inclination | 52.0° | ||||||||||||
Period | 104.30 minutes | ||||||||||||
Instruments | |||||||||||||
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Explorer 16, also called S-55B, was a NASA satellite launched as part of the Explorer program. Explorer 16 was launched on 16 December 1962, at 14:33:04 GMT, [1] from Wallops Flight Facility, Virginia, with a Scout X-3. [3]
Explorer 16 was the second in the series of micrometeoroid satellites orbited by NASA. Its purpose was to obtain data on the near-Earth meteoroid environment, thus providing an accurate estimate of the probability of penetration in spacecraft structures by meteoroids and allowing a more confident definition of the relationship between penetration flux and material thickness to be derived. [3]
The cylindrically shaped spacecraft, about 61 × 192 cm (24 × 76 in), with a mass of 100.8 kg (222 lb), was built around the burned-out fourth stage of the Scout launch vehicle that remained as part of the orbiting satellite. [3]
Explorer 16 carried stainless steel pressurized-cell penetration detectors, impact detectors, capacitor detectors, and cadmium sulfide cell detectors to obtain data on the size, number, distribution, and momentum of dust particles in the near-Earth environment. [3]
This micrometeorite detector consisted of two cadmium-sulfide cells with a total effective area of 48-cm2. Each cell was shielded by a microthin sheet of polymer plastic coated with aluminized Mylar 0.00063 cm (0.00025 in) thick. The detectors were mounted at the end of the cylindrical satellite casing just ahead of the antennas. When a micrometeoroid pierced the shield, it admitted light to the cell and changed the cell's resistance. Resistance was calibrated to the size of the micrometeoroid. Data were obtained from cell A for 20 days and from cell B for 55 days. [4]
This experiment was one of five micrometeorite detectors. There were 46 wire grid detectors consisting of a winding of five copper wires, 52-and 76-microns thick, mounted on 3.68 × 17.8 cm (1.45 × 7.01 in) rectangular melamine cards, to obtain measurements of micrometeoroid impact. Fourteen of the cards were wound with 0.05-mm wire and 32 cards with 0.076-mm wire, providing a total exposed area of 0.3 m2 to penetration by micrometeoroids. When a micrometeoroid broke the wires, the lowered resistance level of an electronic circuit was recorded. Impacts were measured separately on the satellite's two telemeters and were then relayed for transmission to Earth. During the 7.5 months in which the experiment transmitted useful data, telemeter A gave no indication of a break in either the 52-micron or the 76-micron copper wires on the card detectors. Telemeter B recorded one break in the 52-micron and 76-micron wire on 28 June 1963, and one in the 76-micron wire on 13 July 1963. [5]
This experiment was one of five micrometeorite detectors. Sixty foil gauge detectors, each in the shape of an equilateral triangle with a 11.60 cm (4.57 in) base, were installed around the forward usable half of the fourth-stage launch vehicle support structure. Each detector consisted of a circuit obtained by an electrochemical deposition process, about 2.3E-3-mm thick attached to 0.025-mm Mylar and mounted on the underside of 304 stainless steel skin samples. Twenty-four of the skin samples were 0.025-mm thick, and four were 0.15-mm thick. The experiment utilized thin grids of conducting gold deposited on the bottom surface of three stainless steel sheets of different thickness to record micrometeoroid penetration. A particle penetrating the steel sheet would almost invariably break one of the current channels underneath, lowering its resistance level and recording the penetration. Six penetrations were recorded in the 25-micron stainless steel sheet, and one penetration was indicated in the 152-micron stainless steel sheet. The experiment functioned well in the 7.5 months in which the satellite transmitted useful micrometeoroid data. [6]
This experiment was one of five micrometeorite detectors. It used a piezoelectric impact detector to measure micrometeoroid population in a momentum range somewhat higher than that of previous measurements, where few data exist. The detectors, acoustically decoupled from the satellite structure, were mounted at the end of the cylindrical satellite casing near the antennas. The detectors provided a total of 0.35 m2 of area exposed to micrometeoroids. The momentum of a micrometeoroid impacting on the detector assembly was converted into an electrical impulse. The detector had three levels of sensitivity. Data from the impact detectors were correlated with those of micrometeoroid effects on materials in the pressurized cell experiment. The impact detector sent useful data for 7.5 months. By 1 July 1963, 15,000 meteoroid impacts had been recorded by the sensors. [7]
This experiment was one of five micrometeorite detectors. It utilized pressurized cells shaped like half cylinders with walls of 25-, 51-, and 127-micron-thick beryllium copper to record micrometeoroid impacts. The cells contained helium gas held under pressure. As a micrometeoroid punctured the cell wall, it released the gas and dropped the pressure. This drop in pressure activated an electronic circuit and transmitted this information to Earth. The pressurized-cell sensors were divided into two identical groups that were telemetered separately on the two telemeters. During the 7.5 months in which the experiment transmitted useful data, 44 punctures were indicated in the one hundred 25-micron beryllium copper walls, and none of the twenty 127-micron beryllium copper sensors was punctured. The puncture rate for the 25-micron material was 0.32 puncture per m2 per day, and the puncture rate for the 51-micron material was 0.19 puncture per m2 per day. [8]
The spacecraft operated satisfactorily during its 7.5 months life (16 December 1962 to July 1963), and all mission objectives were accomplished. [3]
Explorer 1 was the first satellite launched by the United States in 1958 and was part of the U.S. participation in the International Geophysical Year (IGY). The mission followed the first two satellites the previous year; the Soviet Union's Sputnik 1 and Sputnik 2, beginning the Cold War Space Race between the two nations.
Vanguard 3 is a scientific satellite that was launched into Earth orbit by the Vanguard SLV-7 on 18 September 1959, the third successful Vanguard launch out of eleven attempts. Vanguard rocket: Vanguard Satellite Launch Vehicle-7 (SLV-7) was an unused Vanguard TV-4BU rocket, updated to the final production Satellite Launch Vehicle (SLV).
Explorer 2 was an American unmanned space mission within the Explorer program. Intended to be a repetition of the previous Explorer 1 mission, which placed a satellite into medium Earth orbit, the spacecraft was unable to reach orbit due to a failure in the launch vehicle during launch.
Explorer 35,, was a spin-stabilized spacecraft built by NASA as part of the Explorer program. Designed for the study of the interplanetary plasma, magnetic field, energetic particles, and solar X-rays, from lunar orbit.
Explorer 6, or S-2, was a NASA satellite, launched on 7 August 1959, at 14:24:20 GMT. It was a small, spheroidal satellite designed to study trapped radiation of various energies, galactic cosmic rays, geomagnetism, radio propagation in the upper atmosphere, and the flux of micrometeorites. It also tested a scanning device designed for photographing the Earth's cloud cover. On 14 August 1959, Explorer 6 took the first photos of Earth from a satellite.
Explorer 7 was a NASA satellite launched on 13 October 1959, at 15:30:04 GMT, by a Juno II launch vehicle from Cape Canaveral Air Force Station (CCAFS) to an orbit of 573 × 1,073 km (356 × 667 mi) and inclination of 50.27°. It was designed to measure solar X-ray and Lyman-alpha flux, trapped energetic particles, and heavy primary cosmic rays. Secondary objectives included collecting data on micrometeoroid penetration, molecular sputtering and studying the Earth-atmosphere heat balance.
The Pegasus Project was a NASA initiative to study the frequency of micrometeorite impacts on spacecraft by means of a constellation of three satellites launched in 1965. All three Pegasus satellites were launched by Saturn I rockets, and remained connected with their upper stages.
Explorer 8 was a NASA research satellite launched on 3 November 1960. It was intended to study the temporal and spatial distribution of the electron density, the electron temperature, the ion concentration, the ion mass, the micrometeorite distribution, and the micrometeorite mass in the ionosphere at altitudes between 400 km (250 mi) and 1,600 km (990 mi) and their variation from full sunlit conditions to full shadow, or nighttime, conditions.
Explorer 14, also called EPE-B or Energetic Particles Explorer-B, was a NASA spacecraft instrumented to measure cosmic-ray particles, trapped particles, solar wind protons, and magnetospheric and interplanetary magnetic fields. It was the second of the S-3 series of spacecraft, which also included Explorer 12, 14, 15, and 26. It was launched on 2 October 1962, aboard a Thor-Delta launch vehicle.
Explorer 12, also called EPE-A or Energetic Particles Explorer-A and as S3), was a NASA satellite built to measure the solar wind, cosmic rays, and the Earth's magnetic field. It was the first of the S-3 series of spacecraft, which also included Explorer 12, 14, 15, and 26. It was launched on 16 August 1961, aboard a Thor-Delta launch vehicle. It ceased transmitting on 6 December 1961 due to power failure.
Explorer 26 was a NASA satellite launched on 21 December 1964, as part of NASA's Explorer program. Its primary mission was to study the Earth's magnetic field.
Explorer S-55 was an American satellite launched by NASA on 30 June 1961, as part of the Explorer program. Explorer S-55, was launched using a Scout X-1 launch vehicle from the Wallops Flight Facility (WFF). Its mission was to evaluate the launch vehicle, and investigate micrometeoroid impact and penetration. The mission failed because the third stage failed to ignite and the spacecraft did not achieve orbit.
Explorer 13,, was a NASA satellite launched as part of the Explorer program on 25 August 1961, at 18:29:44 GMT, from Wallops Flight Facility (WFF), Virginia.
Explorer 15, also called EPE-C or Energetic Particles Explorer-C, was a NASA satellite launched as part of the Explorer program. Explorer 15 was launched on 27 October 1962, at Cape Canaveral Air Force Station, Florida, United States, with a Thor-Delta A.
Explorer 21, also called IMP-B, IMP-2 and Interplanetary Monitoring Platform-2, was a NASA satellite launched as part of Explorer program. Explorer 21 was launched on 4 October 1964, at 03:45:00 GMT from Cape Canaveral (CCAFS), Florida, with a Thor-Delta C launch vehicle. Explorer 21 was the second satellite of the Interplanetary Monitoring Platform, and used the same general design as its predecessor, Explorer 18 (IMP-A), launched the previous year, in October 1964. The following Explorer 28 (IMP-C), launched in May 1965, also used a similar design.
Explorer 23 was the last of three S-55 NASA micrometeoroid satellites launched as part of the Explorer program. Its purpose was to obtain data on the near-earth meteoroid environment, thus providing an accurate estimate of the probability of penetration in spacecraft structures by meteoroids and allowing a more confident definition of the penetration flux-material thickness relation to be derived.
Explorer 41, also called as IMP-G and IMP-5, was a NASA satellite launched as part of Explorer program. Explorer 41 as launched on 21 June 1969 on Vandenberg AFB, California, with a Thor-Delta E1 launch vehicle. Explorer 41 was the seventh satellite launched as part of the overall Interplanetary Monitoring Platform series, though it received the post-launch designation "IMP-5" because two previous flights had used the "AIMP" designation instead. It was preceded by the second of those flights, Explorer 35, launched in July 1967. Its predecessor in the strict IMP series of launches was Explorer 34, launched in May 1967, which shared a similar design to Explorer 41. The next launch was of an IMP satellite was Explorer 43 in 1971.
Solrad 10, also known Explorer 44, NRL-PL 165 and Explorer SE-C, was one of the SOLRAD series designed to provide continuous coverage of wavelength and intensity changes in solar radiation in the UV, soft and hard X-ray regions. The satellite also mapped the celestial sphere using a high-sensitivity X-ray detector. Information collected was expected to contribute to a better understanding of the physical processes involved in solar flares and other solar activity, and the potential effects of this activity on short-wave communications, as well as on future human space travel. For the period of July 1971 to June 1973, the core memory data of Explorer 44 were used rather than those from Explorer 37. The Explorer 44 core memory failed on 11 June 1973, and Explorer 37 was heavily used until 25 February 1974, when the gas supply of the attitude control system was exhausted.
Explorer 46,, was a NASA satellite launched as part of Explorer program.
Ever since the beginning of the space age satellites and space probes performed space dust measurements. The goal was, initially, to quantify the hazard of meteoroid impacts onto space vehicles. Samples returned to Earth by the Apollo astronauts demonstrated that the lunar surface is peppered by microcraters generated by high speed impacts of cosmic dust particles. Their analysis provided a measurement of the flux of interplanetary dust particles. The later goal of dust measurements was the exploration of the dust environments throughout interplanetary space, within planetary systems, and, today, it is to analyze planetary bodies from which dust particles originate. The development of instrument went from simple and small but noisy microphone detectors, over large and reliable multi-coincidence dust detectors to sophisticated dust analyzers that determine the composition of individual dust particles.