{"projectId":14711,"project":{"projectId":14711,"title":"Methane Lidar Transmitter Development for Space","startDate":"2013-10-01","startYear":2013,"startMonth":10,"endDate":"2018-09-01","endYear":2018,"endMonth":9,"programId":153,"program":{"ableToSelect":false,"acronym":"GSFC IRAD","isActive":true,"description":"<p>Goddard&#39;s IRAD program is managed under Goddard&#39;s Office of Chief Technologist.&nbsp; Activities are coordinated in collaboration with the Sciences and Exploration Directorate; Applied Engineering and Technology Directorate; Flight Projects Directorate; Wallops Flight Facility; New Opportunites Office; SBIR/STTR program; Goddard Strategic Partnerships Office; and the Export Compliance Office.</p><p>IRAD provides&quot;seed funding&quot; to develop concepts, reduce technology risk, and advance human capital and technological capabilities.&nbsp; The program is highly competitive, opportunity-driven, and 100% strategically aligned with NASA&#39;s and GSFC&#39;s strategic priorities.&nbsp; A significant portion of the program is focused on Early Stage Innovations for high-risk, strategically aligned, potential high-payoff technologies that are longer-term or lower TRL.</p>","parentProgram":{"ableToSelect":false,"acronym":"IRAD","isActive":true,"programId":87,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Center Independent Research & Development","manageGaps":false,"acronymOrTitle":"IRAD"},"parentProgramId":87,"programId":153,"responsibleMd":{"organizationId":4910,"organizationName":"Mission Support Directorate","acronym":"MSD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4910,"title":"Center Independent Research & Development: GSFC IRAD","manageGaps":false,"acronymOrTitle":"GSFC IRAD"},"acronym":"","description":"<!DOCTYPE html PUBLIC \"-//W3C//DTD XHTML 1.0 Strict//EN\"            \"http://www.w3.org/TR/xhtml1/DTD/xhtml1-strict.dtd\"> <p>The objective of this work is to advance the technology readiness  level (TRL) of lidar system to enable global Methane (CH<sub>4</sub>)  and water vapor (H<sub>2</sub>O) measurements with sufficient  coverage, sensitivity, and precision to address pressing science  questions for climate-carbon interaction. Methane (CH<sub>4</sub>) is  the second most important anthropogenic greenhouse gas with  approximately 25 times the radiative forcing of CO<sub>2</sub> per  molecule. Natural sources of CH<sub>4</sub> are dominated by wetland  emissions in the tropics and Arctic and sub-Arctic boreal regions,  with additional contributions from termites, ruminants, ocean biology,  and a geological source of unknown significance. Natural sources  account for about one-third of the emission total. The wetland source  is particularly variable, linked to temperature, precipitation, and  surface hydrological changes. Better characterization of the wetland  source clearly requires reliable CH<sub>4</sub> measurements in the  often-cloudy tropics and over partially inundated land surfaces and  open water. Another important science question is in the potential  release of large amounts of stored organic carbon as CH<sub>4</sub>  and CO<sub>2</sub> from thawing Arctic permafrost soils, which is  cause for concern as a rapid, positive greenhouse gas/climate  feedback. In addition, large but greatly uncertain amounts of  CH<sub>4</sub> are sequestered as gas hydrates in shallow oceans and  permafrost soils, which are also subject to potential rapid release.  Although these boreal, phase-change driven sources are not yet  estimated to be large, their potential magnitude and rapid growth  dictate that measurement systems need to be put in place for early  detection. Because CH<sub>4</sub> fluxes, as well as chemical loss,  are tightly coupled to hydrology, coordinated measurement of both  CH<sub>4</sub> and H<sub>2</sub>O are highly desired. Precise,  seasonal measurements with coverage at high latitudes (i.e., in low  sun to dark conditions) are required. Our proposed laser remote  sensing technology will be a key step in fostering measurements of  CH<sub>4</sub> and H<sub>2</sub>O with sufficient coverage, sampling,  and precision to address major science questions.</p> <p>Our proposed laser remote sensing technology will be a key step in  fostering measurements of CH<sub>4</sub> and H<sub>2</sub>O with  sufficient coverage, sampling, and precision to address these and  other science issues. The benefit to future Earth Science missions is  that the proposed technology enables global CH<sub>4</sub>  measurements to be made where they are really needed: in the absence  of sunlight (i.e., at night and at high latitudes in all seasons), in  the presence of scattered or optically thin clouds and aerosols, over  land and water surfaces, and with higher accuracy and precision than  currently available. These qualities are precisely those that make the  corresponding H<sub>2</sub>O measurements a valuable addition to the  current operational suite for weather and climate analysis. The  measurements will help satisfy the critical scientific need to  understand the behavior of greenhouse gases as they contribute to  climate change as well as to meet pressing national needs for  development of a national carbon monitoring system serving science,  policy-makers, and stakeholders.</p> <p>The end goal of the project would be to demonstrate the readiness of  the a CH<sub>4</sub> trace gas lidar instrument for space flight. The  target wavelengths and energies are ~1.65 µm and energy is ~500 µJ.   The specific objectives of this project are to:</p> <ol>  <li>Improve the tunability architecture of the seed laser(s) using two   different designs.<ol>    <li>The first design uses a DBR laser at 1651 nm to be delivered     under an STMD Game Changing Technology program.</li>    <li>The second design uses a novel approach: single or dual     sideband (SSB/DSB) tuning. It has the potential to significantly     simplify the seed laser design and uses existing DFB lasers.</li></ol></li>  <li>Demonstrate 500 µJ in Er:YGG/Er:YAG with narrow linewidth.</li>  <li>Reduce the size and complexity of the existing OPO</li>  <li>Use the tunable seed from objective 1 with the OPO and Er:YAG from   objectives 2 and 3 to demonstrate open path CH<sub>4</sub>   measurements and correlate them with an in-situ calibrated   instrument (Picarro in-situ CH<sub>4</sub> analyzer).</li></ol>","benefits":"<!DOCTYPE html PUBLIC \"-//W3C//DTD XHTML 1.0 Strict//EN\"                       \"http://www.w3.org/TR/xhtml1/DTD/xhtml1-strict.dtd\"> <p>Orbital or sub-orbital Earth Venture missions or a future ASCENDS   mission to measure greehouse gas mixing ratios in the atmosphere.</p> <p>Space flight laser technology 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