ANNA 1B

from Wikipedia, the free encyclopedia
ANNA 1B
ANNA 1B
Country: United StatesUnited States United States
Operator: US Air Force, US Navy, NASA, US Army
COSPAR-ID : 1962-060A
Mission dates
Dimensions: 161 kg
Size: 91 cm diameter
Begin: October 31, 1962
Starting place: CC LC-17
Launcher: Thor Able star
Orbit data
Rotation time : 107.9 minutes
Orbit inclination : 50.1 °
Apogee height 1182 km (initially)
Perigee height 1076 km
Eccentricity : 0.007

ANNA 1B was a geodetic earth satellite launched from Florida on October 31, 1962. In addition to NASA, it was operated by the three US armed forces. His name is composed of the initials of the operators together ( A irforce, N avy, N ASA, A rmy).

As a prototype of an active or flashlight satellite , ANNA 1B was supposed to serve to investigate the exact figure of the earth and the earth's gravitational field and for this purpose emitted short series of very bright flashes of light. The lightning bolts were photographed by satellite cameras on ground stations in front of the star background, so that the observations of distant stations were synchronized with an accuracy of 1/1000 s by the timer in the satellite.

The satellite also had the SECOR measurement system for distance measurements with microwaves for the first time . The power supply for all systems was provided by solar cells and batteries.

Web links

swell

  • Heinz Mielke: Lexicon of Space Travel , 6th edition, transpress VEB Verlag für Verkehrwesen, Berlin, 1980
  • Günter Seeber: Satellite geodesy , Verlag de Gruyter, Berlin 1989

Individual evidence

  1. ANNA 1B in the NSSDCA Master Catalog , accessed on August 4, 2014 (English).