← Back to Patent Explorer
US3231224A Expired / Lapsed US ⏱️ 0.0 years remaining

Fluid thrust attitude control system for space vehicles

Assignee: Bolkow GmbH
•
Filing: 1964-01-23
•
Granted: 1966-01-25
•
Expires: 1984-01-23
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Koelle Dietrich Eckard

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 19:54
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/40; B64G1/402; B64G1/24; B64G1/26; B64G1/401; Y; Y10; Y10T; Y10T137/00; Y10T137/2931; Y10T137/3115; Y10T137/3127

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 104 words
A CONTROL FOR AJDUSTING THE SPACE POSITION OF SPACE VEHICLE PARTICULARLY IN A POWERLESS FLIGHT PHASE, COMPRIING AT LEAST TWO DIAMETRICALLY ARRANGED AND UNIVERSALLY PIVOTAL MAIN AND CONTROL PROPULSION UNITS ADAPTED TO BE MOUNTED ON SAID SPACE VEHICLE, A SECONDARY PROPULSION UNIT SYSTEM WORKINGG INDEPENDENTLY OF GRAVITATION AND ACCLERATION CONDITIONS FOR GENERATING THRUST IMPULSES FOR CONTROLLING THE SPACE POSITION MOUNTED ON EACH OF SAID PIVOTAL MAIN AND CONTROL PROPULSION UNITS IN A POSITION FOR DISCHARGING THRUST GASES FOR THE CONTROL OF THE SPACE VEHICLE, SAID SECONDARY PROPULSION UNIT SYTESM INCLUDING A JET REACTION ELEMENT WHICH IS PIVOTAL WITH SAID MAIN AND CONTROL PROPULSION UNITS.
Claim 2
Dependent Claim 104 words
A CONTROL FOR AJDUSTING THE SPACE POSITION OF SPACE VEHICLE PARTICULARLY IN A POWERLESS FLIGHT PHASE, COMPRIING AT LEAST TWO DIAMETRICALLY ARRANGED AND UNIVERSALLY PIVOTAL MAIN AND CONTROL PROPULSION UNITS ADAPTED TO BE MOUNTED ON SAID SPACE VEHICLE, A SECONDARY PROPULSION UNIT SYSTEM WORKINGG INDEPENDENTLY OF GRAVITATION AND ACCLERATION CONDITIONS FOR GENERATING THRUST IMPULSES FOR CONTROLLING THE SPACE POSITION MOUNTED ON EACH OF SAID PIVOTAL MAIN AND CONTROL PROPULSION UNITS IN A POSITION FOR DISCHARGING THRUST GASES FOR THE CONTROL OF THE SPACE VEHICLE, SAID SECONDARY PROPULSION UNIT SYTESM INCLUDING A JET REACTION ELEMENT WHICH IS PIVOTAL WITH SAID MAIN AND CONTROL PROPULSION UNITS.

References Cited (Backward Citations)

US3097480A Cited
US2621719A Cited
US2711751A Cited
US2988882A Cited
US2947500A Cited
US3048011A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-01-24 1969-07-26 1970-01-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-01-24 1973-07-26 1974-01-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-01-24 1977-07-26 1978-01-25 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag