NASA Langley Research Center, Composite Optics, Inc., and Nyma/ADF have developed jointly a deployable primary mirror for space telescopes that combines over five years of research on deployment of optical-precision structures and over ten years of development of fabrication techniques for optical-precision composite mirror panels and structures. The deployable mirror is directly applicable to a broad class of non-imaging "lidar" (light direction and ranging) telescopes whose figure-error requirements are in the range of one to ten microns RMS. Furthermore, the mirror design can be readily modified to accommodate imaging-quality reflector panels and active panel-alignment control mechanisms for application to imaging telescopes. The present...
The aperture size is the primary limitation on the resolving power of an optical system, so deployab...
In the mid-1990s, NASA plans to orbit a giant telescope, whose aperture may be as great as 30 meters...
There are several possible approaches to designing exoplanet missions: (1) Coronagraphs (2) Interfer...
NASA Langley Research Center, Composite Optics, Inc., and Nyma/ADF have developed jointly a deployab...
High spatial resolution imagery and large apertures go hand in hand but small satellite volume const...
In this thesis, the development of a deployment mechanism for a primary mirror of a space telescope ...
The TU Delft Deployable Space Telescope proposes to meet increasing demand for high spatio-temporal ...
The success of the Hubble Space Telescope created a great interest in the next generation of space t...
This paper describe design and optimize of the lightweight primary mirror assemblies for the space t...
The use of synthetic aperture elements enables the development of telescopes with sub-meter resoluti...
The Hubble Space Telescope, with its 2.4-m primary mirror, enabled notable scientific progress and d...
<p> For its compact size and light weight, space telescope with deployable support structure for it...
International audienceThe need for both high quality images and lightweight structures is one of the...
There is a growing need for large aperture, ultralightweight, deployable optics (mirrors) for variou...
QC 351 A7 no. 79In this report we describe the work carried out under contract F19628-72-C-0047 enti...
The aperture size is the primary limitation on the resolving power of an optical system, so deployab...
In the mid-1990s, NASA plans to orbit a giant telescope, whose aperture may be as great as 30 meters...
There are several possible approaches to designing exoplanet missions: (1) Coronagraphs (2) Interfer...
NASA Langley Research Center, Composite Optics, Inc., and Nyma/ADF have developed jointly a deployab...
High spatial resolution imagery and large apertures go hand in hand but small satellite volume const...
In this thesis, the development of a deployment mechanism for a primary mirror of a space telescope ...
The TU Delft Deployable Space Telescope proposes to meet increasing demand for high spatio-temporal ...
The success of the Hubble Space Telescope created a great interest in the next generation of space t...
This paper describe design and optimize of the lightweight primary mirror assemblies for the space t...
The use of synthetic aperture elements enables the development of telescopes with sub-meter resoluti...
The Hubble Space Telescope, with its 2.4-m primary mirror, enabled notable scientific progress and d...
<p> For its compact size and light weight, space telescope with deployable support structure for it...
International audienceThe need for both high quality images and lightweight structures is one of the...
There is a growing need for large aperture, ultralightweight, deployable optics (mirrors) for variou...
QC 351 A7 no. 79In this report we describe the work carried out under contract F19628-72-C-0047 enti...
The aperture size is the primary limitation on the resolving power of an optical system, so deployab...
In the mid-1990s, NASA plans to orbit a giant telescope, whose aperture may be as great as 30 meters...
There are several possible approaches to designing exoplanet missions: (1) Coronagraphs (2) Interfer...