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ESSA-6 - Wikipedia

From Wikipedia, the free encyclopedia

ESSA 6
Spacecraft properties

Names	TOS-D

Mission type	Weather
Operator	NASA
COSPAR ID	1967-114A
SATCAT no.	S03035


Launch mass	145 kg (320 lb)


Start of mission
Launch date	November 10, 1967, 18:00 UTC GMT
Rocket	Delta
Launch site	Vandenberg Air Force Base


Orbital parameters
Reference system	Geocentric orbit
Regime	Low Earth orbit
Eccentricity	0.00498
Perigee altitude	1,410 km (880 mi)
Apogee altitude	1,488 km (925 mi)
Inclination	102.12°
Period	114.82 minutes

ESSA program ← ESSA-5 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 299 kilograms (659 lb) 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 108° F/1.8 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.^[1]

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 1,410 kilometers (880 mi) and its apogee was 1,488 kilometers (925 mi).^[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.^[2]

References

^ ^a ^b "ESSA 6". NSSDCA.
^ ^a ^b "ESSA 6 Automatic Picture Transmission (APT) System". NSSDCA.
^ "Launch/Orbital information for ESSA 6". NSSDCA.

This article incorporates public domain material from ESSA 6. National Aeronautics and Space Administration. Retrieved June 4, 2018.

v t e TIROS satellites
TIROS	TIROS-1 TIROS-2 TIROS-3 TIROS-4 TIROS-5 TIROS-6 TIROS-7 TIROS-8 TIROS-9 TIROS-10
TOS	ESSA-1 ESSA-2 ESSA-3 ESSA-4 ESSA-5 ESSA-6 ESSA-7 ESSA-8 ESSA-9
ITOS	TIROS-M NOAA-1 ITOS-B NOAA-2 NOAA-3 NOAA-4 NOAA-5 ITOS-E
TIROS-N	TIROS-N NOAA-6 NOAA-B NOAA-7
Adv. TIROS-N	NOAA-8 NOAA-9 NOAA-10 NOAA-11 NOAA-12 NOAA-13 NOAA-14 NOAA-15 NOAA-16 NOAA-17 NOAA-18 NOAA-19

← 1966

Orbital launches in 1967

1968 →

Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).

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