IN2014DE02967A - - Google Patents

Info

Publication number
IN2014DE02967A
IN2014DE02967A IN2967DE2014A IN2014DE02967A IN 2014DE02967 A IN2014DE02967 A IN 2014DE02967A IN 2967DE2014 A IN2967DE2014 A IN 2967DE2014A IN 2014DE02967 A IN2014DE02967 A IN 2014DE02967A
Authority
IN
India
Prior art keywords
group
panels
flexible members
spacecraft
interface system
Prior art date
Application number
Inventor
Quenten Cook Hugh Jr
R Streett Andrew
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US14/198,126 external-priority patent/US9637248B2/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of IN2014DE02967A publication Critical patent/IN2014DE02967A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays

Abstract

A method and apparatus for deploying a group of panels. An apparatus comprises a group of panels in a folded configuration against a side of a 5 spacecraft, a group of flexible members connected to the group of panels, and an interface system associated with the group of panels and the group of flexible members. The interface system is configured to move the group of panels from the folded configuration to a deployed configuration when the group of flexible members is extended from the spacecraft.
IN2967DE2014 2014-03-05 2014-10-17 IN2014DE02967A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/198,126 US9637248B2 (en) 2013-03-15 2014-03-05 Component deployment system

Publications (1)

Publication Number Publication Date
IN2014DE02967A true IN2014DE02967A (en) 2015-09-11

Family

ID=54207253

Family Applications (1)

Application Number Title Priority Date Filing Date
IN2967DE2014 IN2014DE02967A (en) 2014-03-05 2014-10-17

Country Status (3)

Country Link
JP (1) JP6448293B2 (en)
IN (1) IN2014DE02967A (en)
RU (1) RU2678296C2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11155366B2 (en) * 2017-07-21 2021-10-26 The Aerospace Corporation Interlocking, reconfigurable, reconstitutable, reformable cell-based system with nested ring structures
US11643225B2 (en) 2017-07-21 2023-05-09 The Aerospace Corporation Interlocking, reconfigurable, reconstitutable, reformable cell-based space system
GB2571740A (en) 2018-03-07 2019-09-11 Oxford Space Systems Ltd Deployable spacecraft body
US11858664B1 (en) * 2020-07-29 2024-01-02 Lockheed Martin Corporation Spacecraft for aerospace mission

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3541568A (en) * 1968-02-23 1970-11-17 Herman Lowenhar Storable waveguides for electronic systems
US3698958A (en) * 1969-12-03 1972-10-17 Trw Inc Solar panel
JPS49113400A (en) * 1973-02-22 1974-10-29
US4265690A (en) * 1973-09-24 1981-05-05 Herman Lowenhar Method of forming transmission lines using tubular extendible structures
JPS5837209U (en) * 1981-09-02 1983-03-10 三菱電機株式会社 Hoop-rib mesh antenna
JPS5950899A (en) * 1982-09-14 1984-03-24 三浦　公亮 Solar cell device
US4834325A (en) * 1985-03-20 1989-05-30 Space Industries, Inc. Modular spacecraft system
US4747567A (en) * 1985-03-20 1988-05-31 Space Industries, Inc. Spacecraft with articulated solar array
US4725025A (en) * 1986-03-21 1988-02-16 Rca Corporation Deployment system
US5228644A (en) * 1991-05-28 1993-07-20 The United States Of America As Represented By The United States National Aeronautics And Space Administration Solar powered system for a space vehicle
US5578139A (en) * 1995-01-03 1996-11-26 Aec-Able Engineering Co., Inc. Stowable and deployable solar energy concentrator with fresnel lenses
US5927654A (en) * 1997-05-16 1999-07-27 Lockheed Martin Corp. Spacecraft with active antenna array protected against temperature extremes
US5961738A (en) * 1997-07-30 1999-10-05 Aec-Able Engineering Co., Inc. Solar array for satellite vehicles
US6568640B1 (en) * 1999-07-22 2003-05-27 Lockheed Martin Corporation Inflatable satellite design
JP2001099395A (en) * 1999-10-01 2001-04-10 Nippon Telegr & Teleph Corp <Ntt> Unfolding structure
JP3673519B2 (en) * 2003-03-14 2005-07-20 株式会社パテント・サポート機構 Folding sheet manufacturing method and folding mechanism
US7806370B2 (en) * 2006-03-31 2010-10-05 Composite Technology Development, Inc. Large-scale deployable solar array
EP2272761A1 (en) * 2009-06-18 2011-01-12 Astrium Limited Extendable structure
WO2011006506A1 (en) * 2009-07-15 2011-01-20 Aalborg Universitet Foldable frame supporting electromagnetic radiation collectors
JP2012024876A (en) * 2010-07-22 2012-02-09 Makita Corp Tool storage bag
US9048530B2 (en) * 2011-03-09 2015-06-02 Raytheon Company Deployable flat panel array
WO2014024199A1 (en) * 2012-08-08 2014-02-13 Halsband Arie Low volume micro satellite with flexible winded panels expandable after launch

Also Published As

Publication number Publication date
RU2678296C2 (en) 2019-01-24
RU2014144121A (en) 2016-05-20
RU2014144121A3 (en) 2018-06-21
JP6448293B2 (en) 2019-01-09
JP2015168422A (en) 2015-09-28

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