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Gordon L Collyer

from Culpeper, VA
Age ~76
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Also known as:
Collyer Gordon
Phone and address:
16188 Glenhollow Ct, Culpeper, VA 22701
(540) 547-4117
Related to:
Teressa M Collyer, 57Gordon A CainDwight B CollyerJohn G Collyer, 49Bruce Collyer, 80Anna L CollyerLaura W Collyer, 75Michael Baez, 41James R Carben, 98Michele R Collyer, 48Melissa G Webb, 65Laura W Collyer, 76
Connected to:
Breesa R Collyer, 41Chad A Collyer, 45Franklin B Collyer, 87Helen L Collyer, 104Jocelyn E Collyer, 29Jonathon P Collyer, 48Lois E Collyer, 111Martha J Collyer, 61Raymond D Collyer, 52Scott M Collyer, 49

Gordon Collyer Phones & Addresses

  • 16188 Glenhollow Ct, Culpeper, VA 22701 (540) 547-4117
  • Bellevue, WA
  • 3350 Lake Shore Ln, Clearwater, FL 33761 (727) 785-4800
  • 307 Fillmore St, Beverly Hills, FL 34465
  • Herndon, VA
  • Palm Harbor, FL
  • Fairfax, VA
  • 16188 Glenhollow Ct, Culpeper, VA 22701

Work

Position: Executive, Administrative, and Managerial Occupations

Education

Degree: High school graduate or higher

Business Records

Name / Title
Company / Classification
Phones & Addresses
Gordon Collyer
Director
Bayside Community Church of God, Inc
Churches
3380 State Rd 580, Safety Harbor, FL 34695
(727) 669-7212, (727) 669-7312

Publications

Us Patents

Systems And Methods For Semi-Permanent, Non-Precision Inspace Assembly Of Space Structures, Modules And Spacecraft

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US Patent:
7374134, May 20, 2008
Filed:
Aug 29, 2005
Appl. No.:
11/215570
Inventors:
Gordon L. Collyer - Clearwater FL, US
Jeremy Ramos - Clearwater FL, US
Jason Waltuch - St. Petersburg FL, US
Christopher J. Butera - Odessa FL, US
Assignee:
Honeywell International Inc. - Morristown NJ
International Classification:
B64G 1/64
B23K 13/06
US Classification:
2441724, 219 72
Abstract:
Methods and systems for assembling spacecraft in space are provided. A modular spacecraft comprises a plurality of spacecraft modules, wherein each spacecraft module includes one or more of bonding posts and receiving plates mounted to an exterior surface each spacecraft module, wherein the one or more bonding posts and receiving plates are adapted to form one or more of, an electro-weld bond and an adhesive bond, with the one or more receiving plates.

Spacecraft Grapple Assembly And Docking System Employing The Same

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US Patent:
20090001221, Jan 1, 2009
Filed:
Jun 29, 2007
Appl. No.:
11/771597
Inventors:
Gordon L. Collyer - Clearwater FL, US
Assignee:
HONEYWELL INTERNATIONAL, INC. - Morristown NJ
International Classification:
B64G 1/64
US Classification:
2441724
Abstract:
A spacecraft docking system configured to permit the docking of a spacecraft to a target object is provided. The docking system includes a grapple and docking interface, which is mounted on the target object. The grapple includes a body coupled to the spacecraft and at least one latching wing coupled to the body. The at least one latching wing is movable between a retracted position and an extended position, and configured to move into the extended position and latch onto the docking interface when the grapple is inserted therein.

Reducing Satellite Weight And Cost

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US Patent:
59314192, Aug 3, 1999
Filed:
Aug 7, 1997
Appl. No.:
8/908352
Inventors:
Gordon L. Collyer - Clearwater FL
Assignee:
Honeywell Inc. - Minneapolis MN
International Classification:
B64G 100
US Classification:
244158R
Abstract:
Satellites are launched to a first orbit on a launch rocket. The satellites are connected together, forming a satellite cluster, that is propelled from the first orbit to a higher mission orbit by thrustors on each satellite. The satellite cluster is formed so that satellite cluster rotation from aerodynamic drag on the individual satellites is minimized. The thrustors are sequenced to control satellite cluster attitude during the transition to the second altitude. At the second altitude, the satellites are separated from the satellite cluster and propelled to their mission orbits using their own thrustors and attitude system.

Consolidated Vehicle Propulsion Control Using Integrated Modular Avionics

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US Patent:
20140121862, May 1, 2014
Filed:
Nov 1, 2012
Appl. No.:
13/666565
Inventors:
- Morristown NJ, US
Mitch Fletcher - Glendale AZ, US
Gordon Collyer - Culpeper VA, US
Richard Willis - Largo FL, US
Pat Resing - Seminole FL, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
B64C 19/00
US Classification:
701 3
Abstract:
A vehicle is provided. The vehicle may include, but is not limited to, a virtual backplane, a vehicle management computer communicatively coupled to the first virtual backplane and having a first predetermined schedule, a consolidated propulsion controller communicatively coupled to the virtual backplane and having a second predetermined schedule different from the first predetermined schedule, at least one engine communicatively coupled to the first virtual backplane, each of the at least one engines having a unique schedule, and at least one control system communicatively coupled to the first virtual backplane, each of the at least one control systems having a unique schedule, wherein each of the vehicle management computer, consolidated propulsion controller, at least one engines and at least one control system are configured to add and consume date from the virtual backplane according to their respective schedules.
Control profile
Gordon L Collyer from Culpeper, VA, age ~76 Get Report