To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

Explorer 52
Hawkeye-1.jpg
Explorer 52 / Hawkeye 1
Names
  • Neutral Point Explorer
  • Hawkeye 1
  • Injun-F
Mission typeSpace physics
OperatorNASA / LaRC
COSPAR ID1974-040A
SATCAT no.07325
Mission duration3 years, 10 months, 24 days
Orbits completed667
Spacecraft properties
ManufacturerUniversity of Iowa Department of Physics and Astronomy
BOL mass22.7 kg (50 lb)
Power36 W
Start of mission
Launch dateJune 3, 1974, 23:09:11 (1974-06-03UTC23:09:11) UTC
RocketScout-E1 S191C[1]
Launch siteVandenberg SLC-5
End of mission
DisposalDeorbited
Decay dateApril 28, 1978 (1978-04-29)
Orbital parameters
Reference systemGeocentric
RegimePolar
Eccentricity0.90127
Perigee altitude469 km (291 mi)
Apogee altitude125,570 km (78,030 mi)
Inclination89.81° to 81.85°
Period3,032.4 minutes
Instruments
 

Explorer 52, also known as Hawkeye 1, Injun F, and the Neutral Point Explorer, was an American satellite launched on June 3, 1974, from Vandenberg Air Force Base on a Scout booster.[2]

Mission

The primary mission objective of Hawkeye 1 (Explorer 52) was to conduct particles and fields investigations of the polar magnetosphere of the earth out to 21 earth radii. Secondary objectives were to make magnetic field and plasma distribution measurements in the solar wind, and to study Type-3 radio emissions caused by solar electron streams in the interplanetary medium. To accomplish these objectives, the spacecraft was instrumented with following instruments:

The spacecraft was spin stabilized with a nominal rotational period of 11 s. In celestial coordinates, the positive spin axis coordinates were right ascension 299.4 degrees (plus or minus 1.1 deg) and declination 8.6 deg (plus or minus 1.5 deg). There was no onboard orientation or spin rate control, but the orientation of the spin axis was stable. An optical aspect system operated from launch until September 3, 1974 at which time the optical aspect system was turned off and failed to turn back on. After this period, aspect had to be determined by observing the effect of optical illumination from the sun on a plasma measurement system. Using the sharp peak observed in this data, corrected orientation information was obtained and rewritten to the data records. The complete spacecraft with instruments had a mass of 22.65 kilograms (49.9 lb). Power of 22 to 36 W, depending on solar aspect, was obtained from solar cells. Hawkeye 1 participated in the International Magnetospheric Study (IMS) and during the first half of 1977 data acquisition was confined to IMS special intervals. Data were obtained in real time only, at frequencies of 136 and 400 MHz at 100 bit/s (or 200 bit/s with convolutional coding) plus wideband VLF data.

Specifics

It was designed, built, and tracked by personnel at the Department of Physics and Astronomy, University of Iowa whose sports teams are the Hawkeyes. The spacecraft was launched on June 3, 1974 into a polar orbit with initial apogee over the North Pole and re-entered on April 28, 1978 after 667 orbits or nearly four years of continuous operation. The spacecraft apogee was between 20.28 and 20.92 Earth radii with less than a 1.7 Earth radii perigee. The orbital period was 51.3 hours. During its lifetime, the inclination of the plane of the spacecraft's orbit to the Earth's equator decreased monotonically from 89.81 to 81.85 degrees. The spacecraft's axis of rotation at launch was inertially fixed in its orbital plane, directed towards a constant right ascension and declination, and nearly parallel to the Earth's equatorial plane.

References

  1. ^ "Scout (Algol-3 based)". Gunter's Space Page. Retrieved 22 March 2015.
  2. ^ "NSSDC/COSPAR ID: 1974-040A". NSSDC Master Catalog Search. National Aeronautics and Space Administration. Retrieved 22 March 2015.
  3. ^ NASA Space Science Data Coordinated Archive ELF/VLF Receivers
  4. ^ NASA Space Science Data Coordinated Archive Triaxial Fluxgate Magnetometer
  5. ^ NASA Space Science Data Coordinated Archive Low-Energy Protons and Electrons

External links

This page was last edited on 1 February 2021, at 06:48
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.