ESSA-6 explained

ESSA 6
Names List:TOS-D
Mission Type:Weather
Operator:NASA
Cospar Id:1967-114A
Satcat:S03035
Launch Date:November 10, 1967, 18:00 UTC GMT
Launch Rocket:Delta
Launch Site:Vandenberg Air Force Base
Orbit Reference:Geocentric orbit
Orbit Regime:Low Earth orbit
Orbit Eccentricity:0.00498
Orbit Inclination:102.12°
Orbit Period:114.82 minutes
Apsis:gee
Programme:ESSA program
Previous Mission:ESSA-5
Next Mission:ESSA-7

ESSA 6 (or TOS-D) was a spin-stabilized operational meteorological satellite.[1] Its name was derived from that of its oversight agency, the Environmental Science Services Administration (ESSA).

Details

ESSA 6 had a mass of 299kg (659lb) at the time of launch.

The satellite's electrical power was supplied by about 10,000 1x2 cm solar cells on the cover and 21 nickel-cadmium batteries.

Two redundant wide-angle APT (Automatic Picture Transmission) cameras, mounted on opposite sides and perpendicular to the spin axis, captured images. This subsystem was a camera-transmitter setup, designed to transmit real-time daylight images of cloud cover to ground stations. It included two 2.54-cm vidicon cameras with lenses, mounted 180° apart. Each orbit, the cameras captured four or eight images, with picture taking lasting 8 seconds and transmission 200 seconds. The 800-line images were transmitted at 137.5 MHz to local APT stations, with reticle marks on the images to assist with geographical alignment. Each picture covered a 3100 x 3100 km area with 4 km resolution at nadir, with a 30% overlap to ensure complete coverage.[2]

The base featured crossed-dipole antennas for command reception, while a monopole antenna provided telemetry (136.500 MHz) and tracking (136.770 MHz) from the top.

Spin rate was regulated to 10.9 rpm using a Magnetic Attitude Spin Coil (MASC), which interacted with Earth's magnetic field to maintain a stable spin axis normal to the orbital plane, within ±1 degree.

Mission

ESSA 6 was launched on November 10, 1967, at 18:00 UTC, atop a Delta rocket from Vandenberg Air Force Base, California, USA.

ESSA 6 had an inclination of 102.12°, and orbited the Earth once every 114.8 minutes. Its perigee was 1410km (880miles) and its apogee was 1488km (925miles).[3]

The satellite performed normally after launch.

The APT camera system was successful, operating nearly continuously until November 4, 1969 when the spacecraft was deactivated.

Notes and References

  1. Web site: ESSA 6 . NSSDCA.
  2. Web site: ESSA 6 Automatic Picture Transmission (APT) System . NSSDCA.
  3. Web site: Launch/Orbital information for ESSA 6 . NSSDCA.