Explorer 14
Explorer 14|
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| Mission type |
Earth science |
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| Operator |
NASA |
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| Harvard designation |
1962 Beta Gamma 1 |
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| SATCAT № |
432 |
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| Mission duration |
10 months |
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| Spacecraft properties |
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| Manufacturer |
Goddard Space Flight Center |
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| Launch mass |
40 kilograms (88 lb) |
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| Start of mission |
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| Launch date |
October 2, 1962, 22:11:30 (1962-10-02UTC22:11:30Z) UTC |
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| Rocket |
Delta A |
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| Launch site |
Cape Canaveral LC-17B |
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| End of mission |
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| Last contact |
August 11, 1963 (1963-08-12) |
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| Decay date |
May 25, 1988 |
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| Orbital parameters |
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| Reference system |
Geocentric |
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| Regime |
Highly elliptical |
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| Semi-major axis |
78,707 kilometres (48,906 mi) |
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| Eccentricity |
0.8389330 |
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| Perigee |
2,601.0 kilometers (1,616.2 mi) |
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| Apogee |
96,189.0 kilometers (59,769.1 mi) |
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| Inclination |
42.80 degrees |
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| Period |
2184.60 minutes |
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| RAAN |
212.21 degrees |
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| Mean anomaly |
333.98 degrees |
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| Mean motion |
0.6673 |
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| Epoch |
16 April 1965, 20:39:58 UTC |
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| Revolution number |
122 |
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Explorer 14 is a spin-stabilized, solar-cell-powered spacecraft instrumented to measure cosmic-ray particles, trapped particles, solar wind protons, and magnetospheric and interplanetary magnetic fields. A 16-channel PFM/PM time-division multiplexed telemeter was used. The time required to sample the 16 channels (one frame period) was 0.323 s. Half of the channels were used to convey eight-level digital information, and the others were used for analog information. During ground processing of the telemetered data, the analog information was digitized with an accuracy of 1/100 of full scale. One analog channel was subcommutated in a 16-frame-long pattern and was used to telemeter spacecraft temperatures, power system voltages, currents, etc. A digital solar aspect sensor measured the spin period and phase, digitized to 0.041 s, and the angle between the spin axis and sun direction to about 3-degree intervals.[1][2]
Experiments
There were eight experiments done on the Explorer 14 during its mission.[3]
- Proton Analyzer
- Fluxgate Magnetometers
- Trapped Particle Radiation
- Cosmic Rays
- Proton-Electron Scintillation Detector
- Solar Aspect Sensor
- Electrolytic Timer Experiment
- Solar Cell Damage Experiment
References
This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.
External links
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- Italics indicates probes that failed to deploy or otherwise malfunctioned · ‡ indicate missions yet to launch.
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| | | Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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