Paul R. Stysley
Goddard Space Flight Center
Network
Latest external collaboration on country level. Dive into details by clicking on the dots.
Publication
Featured researches published by Paul R. Stysley.
Applied Optics | 2004
Donald B. Coyle; Richard B. Kay; Paul R. Stysley; Demetrios Poulios
A highly efficient, diode-pumped, Nd:YAG laser is described. The oscillator utilizes an unstable resonator design with a Gaussian reflectivity output coupler and a side-pumped zigzag slab gain medium. The laser produces 18-mJ, 10-ns pulses at a repetition rate of 242 Hz in a near-TEM00 mode with an optical efficiency of up to 14%. An extended performance test was recently concluded in which the transmitter operated at reduced output for more than 4.8 x 10(9) shots with no optical damage. Design criteria, beam quality, and lifetime data are presented.
Proceedings of SPIE | 2012
Michael A. Krainak; James B. Abshire; Jordan Camp; Jeffrey R. Chen; Barry Coyle; Steven X. Li; Kenji Numata; Haris Riris; Mark A. Stephen; Paul R. Stysley; Guangning Yang; Anthony W. Yu
NASA is currently developing several Earth science laser missions that were recommended by the US National Research Council (NRC) Earth Science Decadal Report. The Ice Cloud and Land Elevation Satellite-2 (ICESat-2) will carry the Advanced Topographic Laser Altimeter System (ATLAS) is scheduled for launch in 2016. The Active Sensing of CO2 Emissions over Nights, Days, and Seasons (ASCENDS) mission and will measure column atmospheric CO2 concentrations from space globally. The Gravity Recovery And Climate Experiment (GRACE) Follow-On (GRACEFO) and GRACE-2 missions measure the spatially resolved seasonal variability in the Earths gravitational field. The objective of the Lidar Surface Topography (LIST) mission is to globally map the topography of the Earths solid surface with 5 m spatial resolution and 10 cm vertical precision, as well as the height of overlying covers of vegetation, water, snow, and ice. This paper gives an overview of the laser transmitter and receiver approaches and technologies for several future missions that are being investigated by the NASA Goddard Space Flight Center.
Proceedings of SPIE | 2016
Paul R. Stysley; D. Barry Coyle; Greg B. Clarke; Erich Frese; Gordon Blalock; Peter Morey; Richard B. Kay; Demetrios Poulios; Michael J. Hersh
The Lasers and Electro-Optics Branch at Goddard Space Flight Center has been tasked with building the Lasers for the Global Ecosystems Dynamics Investigation (GEDI) Lidar Mission, to be installed on the Japanese Experiment Module (JEM) on the International Space Station (ISS)1. GEDI will use three NASA-developed lasers, each coupled with a Beam Dithering Unit (BDU) to produce three sets of staggered footprints on the Earths surface to accurately measure global biomass. We will report on the design, assembly progress, test results, and delivery process of this laser system.
Proceedings of SPIE | 2015
Donald B. Coyle; Paul R. Stysley; Demetrios Poulios; Greg Clarke; Richard B. Kay
The Global Ecosystems Dynamics Investigation (GEDI) Lidar, to be installed aboard the International Space Station in early 2018, will use 3 NASA laser transmitters to produce 14 parallel tracks of 25 m footprints on the Earths surface. A global set of systematic canopy measurements will be derived, the most important of which are vegetation canopy top heights and the vertical distribution of canopy structure. Every digitized laser pulse waveform will provide 3-D biomass information for the duration of the mission. A total of 5 GEDI-HOMER lasers are to be built (1 ETU + 3 Flight + 1 spare) in-house at NASA-GSFC, and is based on a well-studied architecture, developed over several years in the Lasers and Electro-Optics Branch.
conference on lasers and electro-optics | 2011
Paul R. Stysley; D. Barry Coyle; Richard B. Kay; Robert Frederickson; Demetrios Poulios; Bryan Blair; Stan Scott; Ed Arnold
We update the status of a diode-pumped, Nd:YAG oscillator that is the prototype laser for NASAs DESDynl mission. After completing TRL-6 testing, this laser has fired over 5.5 billion shots in lifetesting.
IEEE Journal of Quantum Electronics | 2011
Richard B. Kay; Demetrios Poulios; Donald B. Coyle; Paul R. Stysley; Gregory B. Clarke
The theory for Gaussian beam pulse propagation in a zigzag slab amplifier with a Gaussian pump distribution is detailed. Provisions are made for amplification of an input signal with an elliptical Gaussian spatial mode by modifying the time-dependent photon transport equations as described by Eggleston Frantz, and Injeyan. A comparison is made with experimental results of a diode-side-pumped zigzag slab amplifier element amplifying a near-Gaussian beam.
Laser Radar Technology and Applications XXIII | 2018
D. Barry Coyle; Demetrios Poulios; Ricardo Arevalo; Greg Clarke; Paul R. Stysley
Ultra-compact, nanosecond-class spaceflight-compatible UV lasers are finding increasing application in laser desorption, excitation, and ionization analytical applications on planetary missions, such as the detection and characterization of potential molecular biosignatures on Mars or icy moon surfaces. A short pulsed, solid state, UV laser is under development with selectable pulse energy capabilities for optimized sample ion production at a planetary surface.
Laser Radar Technology and Applications XXIII | 2018
Paul R. Stysley; Barry Coyle; Erich Frese; Furqan L. Chiragh; Michael J. Hersh; Demetrios Poulios; Greg Clarke; Cynthia Kirchner; Kristen Washington; Gordon Blalock; Kevin Smith; Peter Morey; Juan Lander; Peter Mule; Richard B. Kay
The Global Ecosystems Dynamics Investigation (GEDI) Lidar Mission will employ three lasers systems internally developed, built, and tested by the NASA Goddard Space Flight Center Lasers and Electro-Optics Branch. Once installed on the Japanese Experiment Module (JEM) on the International Space Station (ISS), the lasers, each coupled with a Beam Dithering Unit (BDU) will produce three sets of staggered footprints on the Earths surface to accurately measure global biomass. Each of the lasers is a heritage Nd:Yag solid state design required to put out Q-switched pulses at a rate of 242 Hz with a minimum 10 mJ per pulse at a 1064 nm wavelength. During the project, an engineering test unit (ETU) was also built and tested to pave the way for the laser systems to be used in space. We report on the technical and programmatic requirements that drove the design and development of the lasers. Also presented is an update of the performance of the engineering test unit qualification and life-testing along with the status of the space flight lasers.
Laser Radar Technology and Applications XXIII | 2018
Aleksey Vasilyev; Paul R. Stysley; D. Barry Coyle; Erich Frese; Furqan L. Chiragh; Robert Switzer; Joe Thomas
Flight quality solid-state lasers require a unique and extensive set of testing and qualification processes, both at the system and component levels to insure the lasers promised performance. As important as the overall laser transmitter design is, the quality and performance of individual subassemblies, optics, and electro-optics dictate the final laser unit’s quality. The Global Ecosystem Dynamics Investigation (GEDI) laser transmitters employ all the usual components typical for a diode-pumped, solid-state laser, yet must each go through their own individual process of specification, modeling, performance demonstration, inspection, and destructive testing. These qualification processes as well as the test results for the laser crystals, laser diode arrays, electro-optics, and optics, will be reviewed as well as the relevant critical issues encountered, prior to their installation in the GEDI flight laser units.
Proceedings of SPIE | 2013
D. Barry Coyle; Paul R. Stysley; Jan F. McGarry; Scott M. Hull; Kenneth Getzandanner; Romae P. Young
The mitigation of orbital debris was addressed in the most recent release of the National Space Policy directing space faring agencies to pursue technologies that will “mitigate and remove on-orbit debris.” No matter what abatement technology is developed and deployed, still lacking is the remote sensing infrastructure to locate and track these objects with adequate precision. We propose using GSFCs ground-based laser ranging facility to provide meter-level or better ranging precision on optically passive 10-30 cm orbital debris targets with the goal of improving current predictions up to 85%. The improved location accuracy also has the immediate benefit of reducing costly false alarms in collision predictions for existing assets.