Sensor, earth

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OBJECT TYPE
SPINNING/SATELLITE
DATE
1974
ARTIFACT NUMBER
1989.0039.001
MANUFACTURER
Barnes Engineering Co.
MODEL
CTS/HERMES/ 13-210A
LOCATION
Stamford, Connecticut, United States of America

More Information


General Information

Serial #
10
Part Number
1
Total Parts
2
AKA
N/A
Patents
N/A
General Description
METAL SENSOR CASING/ SYNTHETIC PARTS/ METAL CASE WITH SYNTHETIC PARTS, FOAM PADDING.

Dimensions

Note: These reflect the general size for storage and are not necessarily representative of the object's true dimensions.

Length
35.0 cm
Width
24.0 cm
Height
29.2 cm
Thickness
N/A
Weight
N/A
Diameter
N/A
Volume
N/A

Lexicon

Group
Space Technology
Category
Communications
Sub-Category
N/A

Manufacturer

AKA
Barnes
Country
United States of America
State/Province
Connecticut
City
Stamford

Context

Country
Unknown
State/Province
Unknown
Period
CTS/HERMES PROGRAM WAS INITIATED IN 1971 & SATELLITE OPERATED FROM JAN. 17, 1976 TO NOV. 24, 1979.
Canada
IDENTICAL SPINNING EARTH SENSORS WERE USED ON CTS/HERMES SATELLITE, THE CANADIAN DESIGNED & BUILT SPACECRAFT WHICH EXPLORED USE OF HIGH POWER TRANSPONDERS AT HIGHER FREQUENCIES TO EXPAND COMMUNICATIONS CAPABILITIES IN NORTHERN CANADA.
Function
PART OF ATTITUDE CONTROL SYSTEM USED TO DETERMINE SPIN RATE OF SATEL- LITE DURING TRANSFER ORBIT, WHEN IT WAS STILL ORBITING EARTH. DIGITAL DATA WERETRANSMITTED VIA TELEMETRY TRANSMITTER TO GROUND RECEIVE STATIONS. BASED ON INFO. FROM BOTH SUN & EARTH SENSORS, ENGINEERS FIRED THRUSTERS TO SLOW SPIN RATE & POSITION SATELLITE FOR FIRING APOGEE MOTOR IN ORDER TO PUT SPACECRAFT IN GEOSTATIONARY ORBIT (REF 1)
Technical
EARTH SENSOR IS PART OF COMPLEX ATTITUDE CONTROL SYSTEM COMPRISED OF SEVERAL SENSORS THAT LOOK AT EARTH & TO DETECT ANY CHANGES IN ATTITUDE. SATELLITE'S STABILITY IS CRITICAL IN ALL 3 AXIS BECAUSE ANTENNAS ARE FOCUSED ON SPECIFIC AREAS ON GROUND & SHIFT OF ONE DEGREE COULD MEAN LOSS OF SIGNAL OVER VERY LARGE AREA (1)
Area Notes
Unknown

Details

Markings
PLATE ON SENSOR READING 'SPAR AEROSPACE PRODUCTS LIMITED/ TORONTO ONTARIO CANADA/ CTS-SPINNING EARTH SENSOR/ MFG. NAME BARNES ENGINEERING COM- PANY, STAMFORD, CONN. U.S.A./ MFR. P/N 13-210A SPAR P/N 61043D5-1/ MFR. S/N 010SPAR S/N 010/ DATE OF MFR. 1/2/74 SPAR SPEC. SG.-217'/ PLATE ON CASE READING 'NOMENCLATURE CONTAINER, SHIPPING/ BEC PART NO. 253201-1008-3/ DESIGN ACTIVITY 00430 STOCK NO. None/ MANUFACTURER Zero SERIAL NO. 101/ CONTRACT NO. S/C21665A/ US BARNES ENGINEERING COMPANY STAMFORD, CONN.'/ DECAL ON CASE READING 'GREEN MAPLE/ JOINT CANADA-U.S.A./NASA/ SPACE PROGRAM'/ EMBOSSED '383401-2017- 3' ON SENSOR CASING.
Missing
APPEARS COMPLETE.
Finish
GOLD COLOURED SENSOR CASING WITH YELLOW & RED SYNTHETIC CAPS/ GREY ENAMEL PAINTED CASE WITH BLACK SYNTHETIC, GREY FOAM.
Decoration
SPAR LOGO ON PLATE.

CITE THIS OBJECT

If you choose to share our information about this collection object, please cite:

Barnes Engineering Co., Sensor, earth, 1974, Artifact no. 1989.0039, Ingenium – Canada’s Museums of Science and Innovation, http://collections.ingeniumcanada.org/en/id/1989.0039.001/

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