Search NASASearch

Engineering topics

Horner, Scott D.

Publications and source records attributed to Horner, Scott D..

Advanced Composite Solar Sail System: Demonstrating Deployable Composite Solar Sails for Future Deep Space Small Spacecraft

NASA is developing new deployable structures and materials technologies for solar sail propulsion systems destined for future low-cost deep space missions. Solar sails eliminate the need for conventional rocket propellants, relying instead upon the pressure of sunlight to generate continuous thrust. They can operate indefinitely, limited only by the space environment durability of the solar sail materials and spacecraft electronic systems.At NASA's Langley Research Center in Hampton, Virginia, and NASA's Ames Research Center in California's Silicon Valley, researchers and engineers are planning a mission to demonstrate the next generation of solar sail technology for small interplanetary spacecraft. As part of this development effort, the Advanced Composite Solar Sail System (ACS3) will demonstrate deployment of an approximately 800 square foot (74 square meter) composite boom (mast) solar sail system in low-Earth orbit. This will be the first use of composite booms as well as sail packing and deployment systems for a solar sail in orbit.

composite materials

Advanced Composite Solar Sail System Animation

At NASA's Langley Research Center in Hampton, Virginia, and Ames Research Center in California's Silicon Valley, researchers and engineers are planning a mission to demonstrate the next generation of solar sail technology for small interplanetary spacecraft. As part of this development effort, the Advanced Composite Solar Sail System (ACS3) will demonstrate deployment of an approximately 800 square foot (74 square meter) composite boom solar sail system in low-Earth orbit. This will be the first use of composite booms as well as sail packing and deployment systems for a solar sail in orbit. Also developed for ACS3 is an innovative tape-spool boom extraction system to minimize blossoming, or jamming, of the coiled booms during deployment.

Horner, Scott D.

SOFIA: Science Vision and Current Status

This slide presentation details the science and status of the Stratospheric Observatory for Infrared Astronomy (SOFIA). SOFIA is a 2.5 m Telescope designed to fit into a modified Boeing 747SP aircraft. It will have imaging and spectroscopy from .03 micron to 1.6 mm, emphasizing the obscured infrared spectrum (i.e., 30-300 micron). It will fly between 39,000 to 45,000 feet, above over 99.8 % of the water vapor which obscures the infrared from other ground based telescopes. Since it is on a ground based airplane, the instrumentation can be interchangeable between flights, it can fly anywhere and anytime. Diagrams show an overview of the observatory, the optical layout, and a comparison of SOFIA with the other major IR Imaging spectroscopic Space Observatories. Pictures include a shot of the installation of the primary mirror, and the Telescope instrument interface. Charts show the first generation instruments, and their ranges of spectral observation. Also the presentation reviews the science questions that SOFIA's instruments will assist in reviewing.

Horner, Scott D.

The JWST/NIRCam Coronagraph: Mask Design and Fabrication

The NIRCam instrument on the James Webb Space Telescope will provide coronagraphic imaging from lambda =1-5 microns of high contrast sources such as extrasolar planets and circumstellar disks. A Lyot coronagraph with a variety of circular and wedge-shaped occulting masks and matching Lyot pupil stops will be implemented. The occulters approximate grayscale transmission profiles using halftone binary patterns comprising wavelength-sized metal dots on anti-reflection coated sapphire substrates. The mask patterns are being created in the Micro Devices Laboratory at the Jet Propulsion Laboratory using electron beam lithography. Samples of these occulters have been successfully evaluated in a coronagraphic testbed. In a separate process, the complex apertures that form the Lyot stops will be deposited onto optical wedges. The NIRCam coronagraph flight components are expected to be completed this year.

Coronagraph