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ANNA 1B

ANNA 1B (acronym for "Army, Navy, NASA, Air Force") was a United States satellite launched on October 31, 1962, from Cape Canaveral, on a Thor rocket.

ANNA 1B
Photo of ANNA 1B
Mission typeGeodetic research
OperatorDepartment of Defense / NASA
COSPAR ID1962-060A
SATCAT no.00446
Spacecraft properties
ManufacturerApplied Physics Laboratory[1]
Launch mass161 kilograms (355 lb)
Start of mission
Launch dateOctober 31, 1962, 08:03:00 (1962-10-31UTC08:03Z) UTC
RocketThor-DM21 Able Star
Launch siteCape Canaveral LC-17A
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Semi-major axis7,505.0 kilometers (4,663.4 mi)
Perigee altitude1,081.6 kilometers (672.1 mi)
Apogee altitude1,186.7 kilometers (737.4 mi)
Inclination50.1°
Period107.8 minutes[2]
 

Features edit

 
ANNA 1B track on photography taken by Santiago (Chile) MOTS station on November 11, 1962

ANNA 1B's predecessor launched on May 10, 1962, but failed to reach orbit.[3]

ANNA 1B was a US Navy geodetic satellite launched from Cape Canaveral by a Thor Able Star rocket. The mission profile involved ANNA serving as a reference for making precise geodetic surveys, allowing measurement of the force and direction of the gravity field of Earth, locating the middle of land masses and establishing surface positions.

ANNA 1B was spherically shaped with a diameter of 0.91 meters and a weight of 161 kg. It was powered by a band of solar cells around its equator supported by nickel-cadmium batteries. A communications antenna was wrapped around the spiral surface of the satellite.

The ship's instrumentation included optical systems, radio location, and Doppler radar. The optical system consists of a high intensity beacon which transmits a series of five flashes with a period of 5.6 seconds. This allowed one to accurately measure land masses by ground-to-sky satellite photographs (optical tracking or stellar triangulation). The Doppler radar system could also be programmed from the ground control station allowing geopositioning with an accuracy of 20 meters or less.

References edit

  1. ^ Mark Wade. . Astronautix.com. Archived from the original on 2013-11-08. Retrieved 2016-06-28.
  2. ^ N2YO. Real Time Satellite Tracking. "ANNA 1B". N2yo.com. Retrieved 2016-06-28.
  3. ^ NASA. "ANNA1". Nssdc.gsfc.nasa.gov. Retrieved 2016-06-28.

Bibliography edit

  • Bramschere, Robert G (1980). "A Survey of Launch Vehicle Failures". Spaceflight 22: 351.

External links edit

  • NASA/MOTS OPTICAL OBSERVATIONS OF THE ANNA IB SATELLITE. (PDF)


anna, acronym, army, navy, nasa, force, united, states, satellite, launched, october, 1962, from, cape, canaveral, thor, rocket, photo, mission, typegeodetic, researchoperatordepartment, defense, nasacospar, id1962, 060asatcat, 00446spacecraft, propertiesmanuf. ANNA 1B acronym for Army Navy NASA Air Force was a United States satellite launched on October 31 1962 from Cape Canaveral on a Thor rocket ANNA 1BPhoto of ANNA 1BMission typeGeodetic researchOperatorDepartment of Defense NASACOSPAR ID1962 060ASATCAT no 00446Spacecraft propertiesManufacturerApplied Physics Laboratory 1 Launch mass161 kilograms 355 lb Start of missionLaunch dateOctober 31 1962 08 03 00 1962 10 31UTC08 03Z UTCRocketThor DM21 Able StarLaunch siteCape Canaveral LC 17AOrbital parametersReference systemGeocentricRegimeLow EarthSemi major axis7 505 0 kilometers 4 663 4 mi Perigee altitude1 081 6 kilometers 672 1 mi Apogee altitude1 186 7 kilometers 737 4 mi Inclination50 1 Period107 8 minutes 2 Contents 1 Features 2 References 3 Bibliography 4 External linksFeatures edit nbsp ANNA 1B track on photography taken by Santiago Chile MOTS station on November 11 1962ANNA 1B s predecessor launched on May 10 1962 but failed to reach orbit 3 ANNA 1B was a US Navy geodetic satellite launched from Cape Canaveral by a Thor Able Star rocket The mission profile involved ANNA serving as a reference for making precise geodetic surveys allowing measurement of the force and direction of the gravity field of Earth locating the middle of land masses and establishing surface positions ANNA 1B was spherically shaped with a diameter of 0 91 meters and a weight of 161 kg It was powered by a band of solar cells around its equator supported by nickel cadmium batteries A communications antenna was wrapped around the spiral surface of the satellite The ship s instrumentation included optical systems radio location and Doppler radar The optical system consists of a high intensity beacon which transmits a series of five flashes with a period of 5 6 seconds This allowed one to accurately measure land masses by ground to sky satellite photographs optical tracking or stellar triangulation The Doppler radar system could also be programmed from the ground control station allowing geopositioning with an accuracy of 20 meters or less References edit Mark Wade Anna Astronautix com Archived from the original on 2013 11 08 Retrieved 2016 06 28 N2YO Real Time Satellite Tracking ANNA 1B N2yo com Retrieved 2016 06 28 NASA ANNA1 Nssdc gsfc nasa gov Retrieved 2016 06 28 Bibliography editBramschere Robert G 1980 A Survey of Launch Vehicle Failures Spaceflight 22 351 External links editNASA MOTS OPTICAL OBSERVATIONS OF THE ANNA IB SATELLITE PDF nbsp This article about one or more spacecraft of the United States is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title ANNA 1B amp oldid 1163584600, wikipedia, wiki, book, books, library,

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