Explorer 7
 Explorer 7 satellite | |
| Names | NASA S-1A |
|---|---|
| Mission type | Earth science |
| Operator | NASA |
| Harvard designation | 1959 Iota 1 |
| COSPAR ID | 1959-009A |
| SATCATno. | 00022 |
| Mission duration | 1 year, 10 months and 10 days (achieved) 64 years and 9 months (in orbit) |
| Spacecraft properties | |
| Spacecraft | Explorer VII |
| Spacecraft type | Science Explorer |
| Bus | S-1A |
| Manufacturer | Jet Propulsion Laboratory |
| Launch mass | 41.5 kg (91 lb) |
| Dimensions | 76 × 76 cm (30 × 30 in) |
| Start of mission | |
| Launch date | 13 October 1959, 15:30:04GMT[1] |
| Rocket | Juno II(AM-19A) |
| Launch site | Cape Canaveral,LC-5 |
| Contractor | Army Ballistic Missile Agency |
| Entered service | 13 October 1960 |
| End of mission | |
| Last contact | 24 August 1961 |
| Orbital parameters | |
| Reference system | Geocentric orbit[2] |
| Regime | Low Earth orbit |
| Perigee altitude | 573 km (356 mi) |
| Apogee altitude | 1,073 km (667 mi) |
| Inclination | 50.27° |
| Period | 101.38 minutes |
| Instruments | |
| Ground Based Ionospheric Heavy Primary Cosmic Rays Micrometeorite Solar X-Ray and Lyman-Alpha Radiation Thermal Radiation Trapped Radiation and Solar Protons | |
Explorer program | |
Explorer 7was a NASA satellite launched on 13 October 1959, at 15:30:04GMT,[1]by aJuno IIlaunch vehicle fromCape Canaveral Air Force Station(CCAFS) to an orbit of 573 × 1,073 km (356 × 667 mi) andinclinationof 50.27°.[2]It was designed to measuresolar X-rayandLyman- Alpha flux,trappedenergetic particles,and heavy primarycosmic rays.Secondary objectives included collecting data onmicrometeoroid penetration,molecular sputtering and studying the Earth-atmosphere heat balance.[3]
Satellite description[edit]
The spin-stabilized satellite's external structure consisted of two truncated conicalfiberglassshells joined by a cylindricalaluminumcenter section. The spacecraft was 76 cm (30 in) wide at its equator and about 76 cm (30 in) high with a payload mass of about 41.5 kg (91 lb). The spacecraft was powered by approximately 3000solar cellsmounted on both the upper and lower shells. Additional power was provided by 15 rechargeablenickel-cadmium batteriesthat were positioned on its equator near the outer skin as an aid in maintaining a proper spin rate. Two crossed dipole (1 W, 20-MHz) telemetry antennas projected outward from the center section, and a 108-MHz antenna used for tracking was mounted on the bottom of the lower shell.
Located around the periphery of the center section were fivebolometersfor thermal radiation measurements and threecadmium sulfidemicrometeoroid detector cells. A cylindrical ion chamber (lithium fluoride window) and a beryllium window X-ray chamber were located on opposite sides of the upper cone, and a cosmic-rayGeiger counterwas located on the very top. A primary cosmic-ray ionization chamber was located within the center portion of the upper cone. Communications and tracking were provided by a 108-MHz transmitter at 15-mW designed to operate for 2 months and a 20-MHz transmitter at 600-mW powered by the solar cells designed for cut-off after about one year.[3]
Experiments[edit]
Ground Based Ionospheric[edit]
An all-transistor beacon telemetry transmitter was operated at a fundamental frequency of 19.9915MHz.This transmitter, which was powered by solar cells and rechargeable nickel-cadmium batteries, provided 660-mW of power at the fundamental frequency. It also radiated the second and third harmonics (15-mW each) at 39.9830 and 59.9745-MHz. Beacon receivers were known to have been located inWashington, D.C.,andChicago,Illinois.Interpretation of the changes of beacon signal characteristics between the satellite and the ground station showed irregularities to be present at all times of the day with horizontal dimensions of 5 km (3.1 mi) to 500 km (310 mi). Data were received over a period of 16 months.[4]
Heavy Primary Cosmic Rays[edit]
This experiment was designed to measure the omnidirectional flux of heavy primary cosmic rays in the rigidity range 1 to 15.5GV.Particles with atomic numbers Z >5, Z >8, and Z >15 were counted separately by an ionization chamber in which each incident particle yielded a pulse. Pulse amplitude was substantially independent of the energy of the incident particle but was proportional to the square of its Z value. Each of the three counting rates was determined every 15 seconds. The experiment performed as planned from launch until 25 October 1959. About 80% of the data acquired for the 25 October 1959, to 31 May 1960, period are useful, with most problems occurring in the lowest Z mode. Very little useful data were acquired after 31 May 1960.[5]
Micrometeorite[edit]
Three photoconductingcadmium sulfidecells were used to measuremicrometeoritepenetration and molecular sputtering. The three cells were identical in design and effective area (18 sq mm) and were mounted on amagnesiumplate on the satellite's equator facing outward perpendicular to the satellite's spin axis. The experiment was exposed to the space environment of micrometeorites, trapped radiation, and sputtering for 38 days of active life. The three cells and a thermistor that was included as part of the experiment performed normally. One cell was penetrated on the 16th day by a particle approximately 10 microns in diameter.[6]
Solar X-Ray and Lyman-Alpha Radiation[edit]
The solar X-ray and Lyman- Alpha radiation were measured by means of gas ionization chambers mounted on opposite sides of the upper portion of the double cone configuration of the Explorer 7 satellite. Intensities were monitored in order to obtain a long-term history of solar X-ray andLyman- Alphafluxes and to correlate these with terrestrial atmospheric responses. The two X-ray detectors (2.5 cm (0.98 in) deep) were filled with argon gas and had beryllium windows (.021 g/sq cm) resulting in a sensitivity to X-rays in the 2 to 8Arange. The Lyman- Alpha detectors (on the opposite side), which were circular ionization chambers (1.9 cm (0.75 in) in diameter) filled withnitric oxide gas,hadlithium fluoridewindows. Their sensitivity was in the 1050 to 1350 A interval. The data, however, were impossible to interpret in terms of incident solar radiation due to both the saturation of detector circuits by Van Allen radiation (150 keVelectrons) and electronic difficulties in the feedback amplifier.[7]
Thermal Radiation[edit]
The Explorer 7 thermal radiation experiment was designed to measure incident and reflected solarUV radiationand terrestrialIR radiationin order to obtain a better understanding of the driving forces of the Earth-atmosphere system. The primary instrumentation consisted of five bolometers in the form of hollowsilverhemispheres that were thermally insulated from, but in close proximity to speciallyaluminized mirrors.The hemispheres thereby behaved very much like isolated spheres in space. Two of the hemispheres had black coatings and responded about equally to solar and terrestrial radiation. A third hemisphere, coated white, was more sensitive to terrestrial radiation than to solar radiation. A fourth, which had agold metal surface,was more sensitive to solar radiation than to terrestrial radiation. The fifth hemisphere, protected from direct sunlight, was used to measure the reflected sunlight. A glass-coated bead thermistor was mounted on the top of each hemisphere to measure the temperature. A complete set of four temperature observations and one reference sample required 30 seconds. Thus, in each orbit, about 180 temperature measurements could be obtained. The experiment was a success, and usable data were obtained from launch until 28 February 1961.[8]
Significantly, it also carriedDr. Verner E. Suomi's flat-plateradiometer,improved with the help ofRobert Parent,that took the firstEarth radiation budgetmeasurements from space and initiated the era ofsatellitestudies of theclimate.It made thefirst coarse mapsof "the solar radiation reflected by the Earth and the infrared radiation emitted by the Earth".[9]
Using both satellite observations of the Earth's heat balance andatmosphericcooling rates measured by net flux radiosondes, Suomi established the important role played bycloudsin absorbing radiatedsolar energy.These observations established that Earth's energy budget varies markedly due to the effect of clouds, the surface albedo, and other absorbing constituents. Using these instruments, Suomi and his team discovered that theEarthabsorbed more of theSun's energy than originally thought and demonstrated that it was possible to measure and quantify seasonal changes in the global heat budget. Explorer 7 was unable to detect solar X-rays due to its sensors being saturated by background radiation in theVan Allen radiation belt.[10]
Trapped Radiation and Solar Protons[edit]
Two omnidirectionalGeiger counters(Anton 302 and 112) were used to conduct a comprehensive spatial and temporal monitoring of total cosmic-ray intensity, geomagnetically trapped corpuscular radiation, andsolar protons.The detector was sensitive to protons (E >20 MeV) and electrons (E >30 keV). The experiment operated satisfactorily from launch until 28 February 1961, except for a brief period in September and October 1960.[11]
Launch[edit]
Launch was originally scheduled for late September 1959, but the mission was delayed for a week after aJupiter IRBMtest on an adjacent pad failed shortly after liftoff, causing flying debris to hit Explorer 7's launch vehicle. However, the damage to the booster was minor and could be easily repaired.
Explorer 7 was launched on aJuno IIat 15:31GMTon 13 October 1959 from theAtlantic Missile Rangeinto a 573 × 1,073 km (356 × 667 mi) orbit. On 16 June 1960, NASA announced one of the four frequency modulated subcarriers on the second transmitter had become erratic and the information it was transmitting on 3 of the 7 experiments was no longer intelligible. The tracking beacon ceased transmitting on 5 December 1959. As of September 1960 the orbit was 554 × 1,083 km (344 × 673 mi) with aninclinationof 50.3° and aperiodof 101.2 minutes. Useful real-time data were transmitted from launch through February 1961 and intermittently until 24 August 1961. The spacecraft provided significant geophysical information on radiation and magnetic storms, demonstrated methods of controlling internal temperatures, recorded the first micrometeorite penetration of a sensor in flight, and detected large scale weather patterns.[3]
Mission results[edit]
It transmitted data continuously through to February 1961 and went dead on 24 August 1961. As of 2024[update]It is still in orbit.[12]
See also[edit]
References[edit]
- ^ab"Launch Log".Jonathan's Space Report. 21 July 2021.Retrieved2 November2021.
- ^ab"Trajectory: Explorer 7 (1959-009A)".NASA. 28 October 2021.Retrieved2 November2021.
This article incorporates text from this source, which is in thepublic domain.
- ^abc"Display: Explorer 7 (1959-009A)".NASA. 28 October 2021.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
- ^"Experiment: Ground Based Ionospheric".NASA. 28 October 2021.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
- ^"Experiment: Heavy Primary Cosmic Rays".NASA. 28 October 2021.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
- ^"Experiment: Micrometeorite".NASA. 28 October 2021.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
- ^"Experiment: Solar X-Ray and Lyman-Alpha Radiation".NASA. 28 October 2021.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
- ^"Experiment: Thermal Radiation".NASA. 28 October 2021.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
- ^Kidder, S. Q.; Vonder Haar, T. H. (1995).Satellite Meteorology: An Introduction.Elsevier Science. p. 2.ISBN978-0-08-057200-0.Retrieved5 October2020.
- ^Significant Achievements in Solar Physics 1958-1964.Washington D.C.: NASA. 1966. p. 63.This article incorporates text from this source, which is in thepublic domain.
- ^"Experiment: Trapped Radiation and Solar Protons".NASA. 28 October 2021.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
- ^"U.S. Space Objects Registry".Archived fromthe originalon 30 October 2007.Retrieved2 November2021.This article incorporates text from this source, which is in thepublic domain.
