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US3228628A Expired / Lapsed US ⏱️ 0.0 years remaining

Method and apparatus for magnetically orienting a space vehicle

Assignee: Individual
•
Filing: 1963-04-30
•
Granted: 1966-01-11
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Expires: 1983-04-30
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Abstract

No abstract record available.

Inventors

  • 👤 Talbot A Chubb

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 21:18
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/24; B64G1/32; B64G1/36; B64G1/363; B64G1/366; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1261; Y10T74/1264

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 109 words
A SYSTEM FOR CONTROLLING THE ORIENTATION OF THE AXIS OF ROTATION OF A SPINNING SPACE VEHICLE WITH RESPECT TO A VECTOR DIRECTION COMPRISING: (A) FIRST MEANS FOR SENSING THE RELATIONSHIP OF A VECTOR WITHIN SIAD VEHICLE TO THE EARTH''S MAGNETIC FIELD, (B) SECOND MEANS FOR SENSING THE RELATIONSHIP OF THE EQUATORIAL PLANE OF SAID VEHICLE TO SAID VECTOR DIRECTION, (C) ELECTRONIC CIRCUIT MEANS FOR PROVIDING SEPARATE ELECTRICAL OUTPUTS IN RESPONSE TO SAID SENSED RELATIONSHIPS, AND (D) COIL MEANS FOR APPLYING A TORQUING FORCE TO SAID SPACE VEHICLE IN RESPONSE TO SAID ELECTRICAL OUTPUTS WHEREBY SAID AXIS OF ROTATION IS MOVED TO A POSITION SUBSTANTIALLY PERPENDICULAR TO SAID VECTOR DIRECTION.
Claim 2
Independent Claim 109 words
A SYSTEM FOR CONTROLLING THE ORIENTATION OF THE AXIS OF ROTATION OF A SPINNING SPACE VEHICLE WITH RESPECT TO A VECTOR DIRECTION COMPRISING: (A) FIRST MEANS FOR SENSING THE RELATIONSHIP OF A VECTOR WITHIN SIAD VEHICLE TO THE EARTH''S MAGNETIC FIELD, (B) SECOND MEANS FOR SENSING THE RELATIONSHIP OF THE EQUATORIAL PLANE OF SAID VEHICLE TO SAID VECTOR DIRECTION, (C) ELECTRONIC CIRCUIT MEANS FOR PROVIDING SEPARATE ELECTRICAL OUTPUTS IN RESPONSE TO SAID SENSED RELATIONSHIPS, AND (D) COIL MEANS FOR APPLYING A TORQUING FORCE TO SAID SPACE VEHICLE IN RESPONSE TO SAID ELECTRICAL OUTPUTS WHEREBY SAID AXIS OF ROTATION IS MOVED TO A POSITION SUBSTANTIALLY PERPENDICULAR TO SAID VECTOR DIRECTION.

References Cited (Backward Citations)

No citation records indexed.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-01-10 1969-07-12 1970-01-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-01-10 1973-07-12 1974-01-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-01-10 1977-07-12 1978-01-11 $7700.00 Window Closed / Lapsed

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