FIELD: instrument making.
SUBSTANCE: proposed frame consists of lengthwise, crosswise and diagonal rods interjointed at cross points. Said rods are composite and are jointed together be bimetal rings along their ODs and IDs. Note here that said rods, at their joint with bimetal rings, have lengthwise cutouts made for fringe effect length. Note here that geometrical sizes of composite cylindrical rods, bimetal wings as well as physical and mechanical properties of used material are interrelated by relationships specified in invention claim.
EFFECT: stability of frame linear sizes in irregular temperature field that allows reducing telescope defocusing.
6 dwg
Title | Year | Author | Number |
---|---|---|---|
SPACE TELESCOPE SUPPORTING GIRDER | 2012 |
|
RU2503048C1 |
LOAD-BEARING STRUCTURE FOR SPACE EQUIPMENT | 2015 |
|
RU2610070C1 |
SPACE TELESCOPE MAIN FRAME | 2010 |
|
RU2448878C1 |
POWER ELEMENT OF TRUSS STRUCTURE, FABRICATED BY METHOD OF METALLURGY OF GRANULES, AND CAPSULE FOR ITS PRODUCTION | 2014 |
|
RU2557091C1 |
MESH COMPOSITE HOUSING OF SPACE TELESCOPE | 2019 |
|
RU2724162C1 |
STABLE-SIZE ENCLOSURE | 2008 |
|
RU2373118C1 |
SERVICE SYSTEM MODULE | 2015 |
|
RU2621221C1 |
SPACE VEHICLE | 2017 |
|
RU2673447C9 |
SPACECRAFT OPTICAL-MECHANICAL UNIT ASSEMBLING METHOD | 2015 |
|
RU2610919C1 |
REFLECTOR OF UNFOLDED ANTENNA, ITS TRANSFORMED FRAME, UNFOLDING MECHANISM AND LOCKING MEMBER | 1994 |
|
RU2084994C1 |
Authors
Dates
2011-04-27—Published
2010-03-03—Filed