Zobrazeno 1 - 10
of 13
pro vyhledávání: '"V. Stanley Scott"'
Autor:
Matthew J. McGill, Patrick Selmer, Andrew Kupchock, V. Stanley Scott, John E. Yorks, Shane Wake, William D. Hart, Dennis L. Hlavka
Publikováno v:
Journal of Atmospheric and Oceanic Technology. 31:2482-2497
The Airborne Cloud–Aerosol Transport System (ACATS) is a Doppler wind lidar system that has recently been developed for atmospheric science capabilities at the NASA Goddard Space Flight Center (GSFC). ACATS is also a high-spectral-resolution lidar
Publikováno v:
Journal of Atmospheric and Oceanic Technology. 30:345-352
The Ice, Cloud, and land Elevation Satellite-2 (ICESat-2) mission is currently under development by NASA. The primary mission of ICESat-2 will be to measure elevation changes of the Greenland and Antarctic ice sheets, document changes in sea ice thic
Autor:
David E. Smith, Joseph A. Connelly, Haris Riris, Melanie N. Ott, Anne Marie Novo-Gradac, Peter Liiva, Erwan Mazarico, Xiaoli Sun, David D. Rowlands, Glenn B. Jackson, Thomas W. Zagwodzki, Carlton Peters, Adam Matuszeski, James C. Smith, V. Stanley Scott, Mark H. Torrence, Gregory A. Neumann, Richard B. Katz, Lawrence Ramsey, John F. Cavanaugh, Joseph Paul Swinski, Luis Ramos-Izquierdo, Jan F. McGarry, Glenn Unger, Anthony W. Yu, Craig Coltharp, George B. Shaw, Maria T. Zuber, Ronald S. Zellar, Stephen Schmidt, Igor Kleyner
Publikováno v:
Space Science Reviews. 150:209-241
The Lunar Orbiter Laser Altimeter (LOLA) is an instrument on the payload of NASA's Lunar Reconnaissance Orbiter spacecraft (LRO) (Chin et al., in Space Sci. Rev. 129:391-419, 2007). The instrument is designed to measure the shape of the Moon by mea-
Autor:
James R. Campbell, Dennis L. Hlavka, Ellsworth J. Welton, Connor J. Flynn, David D. Turner, James D. Spinhirne, V. Stanley Scott, I. H. Hwang
Publikováno v:
Journal of Atmospheric and Oceanic Technology. 19:431-442
Publikováno v:
The Review of Laser Engineering. 23:112-118
New technology for compact, eye safe lidar is surveyed. Advances with solid state lasers anddetectors permit efficient lidar designs that meet requirements for full time atmospheric monitoring. Micro pulse lidar is an approach that employs kHz pulse
Autor:
Stephen Schmidt, Peter Liiva, Carlton Peters, V. Stanley Scott, Haris Riris, Michael Rodriguez, Jeffrey Guzek, Luis Ramos-Izquierdo, John F. Cavanaugh, Joseph A. Connelly, William Mamakos
Publikováno v:
Applied optics. 48(16)
The Lunar Orbiter Laser Altimeter (LOLA), developed for the 2009 Lunar Reconnaissance Orbiter (LRO) mission, is designed to measure the Moon's topography via laser ranging. A description of the LOLA optical system and its measured optical performance
Autor:
William Mamakos, Stephen Schmidt, Raymond Trunzo, Jamie Britt, Roger L. Miller, V. Stanley Scott, Luis Ramos-Izquierdo, John F. Cavanaugh
Publikováno v:
Applied optics. 44(9)
The Mercury Laser Altimeter (MLA). developed for the 2004 MESSENGER mission to Mercury, is designed to measure the planet's topography via laser ranging. A description of the MLA optical system and its measured optical performance during instrument-l
Publikováno v:
Applied optics. 41(18)
The new Cloud Physics Lidar (CPL) has been built for use on the NASA ER-2 high-altitude aircraft. The purpose of the CPL is to provide multiwavelength measurements of cirrus, subvisual cirrus, and aerosols with high temporal and spatial resolution. T
Autor:
Stephen P. Palm, James D. Spinhirne, Katherine Manizade, Ronald C. Grush, V. Stanley Scott, James W. Hoffman, John F. Cavanaugh
Publikováno v:
Infrared Detectors and Focal Plane Arrays V.
In August 1997 an infrared spectral imaging radiometer (ISIR) based on uncooled microbolometer array technology was flown on space shuttle mission STS-85. In this paper the design of the instrument and experimental goals are presented, and initial re
Publikováno v:
Optical Remote Sensing of the Atmosphere.
Until recently establishing numbers of continuously operating lidar systems to monitor all cloud and aerosol structure of the atmosphere would have meant large manned instruments and would be largely beyond the realm of feasibility. A program is now