The CLARREO mission addresses the need to provide accurate, broadly acknowledged climate records that can be used
to validate long-term climate projections that become the foundation for informed decisions on mitigation and adaptation
policies. The CLARREO mission accomplishes this critical objective through rigorous SI traceable decadal change
observations that will reduce the key uncertainties in current climate model projections. These same uncertainties also
lead to uncertainty in attribution of climate change to anthropogenic forcing. CLARREO will make highly accurate and
SI-traceable global, decadal change observations sensitive to the most critical, but least understood climate forcing,
responses, and feedbacks. The CLARREO breakthrough is to achieve the required levels of accuracy and traceability to
SI standards for a set of observations sensitive to a wide range of key decadal change variables. The required accuracy
levels are determined so that climate trend signals can be detected against a background of naturally occurring
variability. The accuracy for decadal change traceability to SI standards includes uncertainties associated with
instrument calibration, satellite orbit sampling, and analysis methods. Unlike most space missions, the CLARREO
requirements are driven not by the instantaneous accuracy of the measurements, but by accuracy in the large time/space
scale averages that are necessary to understand global, decadal climate changes.
KEYWORDS: Systems modeling, Taxonomy, Systems engineering, Wind energy, Satellites, Solar radiation models, Atmospheric modeling, Data modeling, Clouds, Climatology
The Group on Earth Observations (GEO) is driving a paradigm shift in the Earth Observation community, refocusing
Earth observing systems on GEO Societal Benefit Areas (SBA). Over the short history of space-based Earth observing
systems most decisions have been made based on improving our scientific understanding of the Earth with the implicit
assumption that this would serve society well in the long run. The space agencies responsible for developing the
satellites used for global Earth observations are typically science driven. The innovation of GEO is the call for
investments by space agencies to be driven by global societal needs. This paper presents the preliminary findings of an
analysis focused on the observational requirements of the GEO Energy SBA. The analysis was performed by the
Committee on Earth Observation Satellites (CEOS) Systems Engineering Office (SEO) which is responsible for
facilitating the development of implementation plans that have the maximum potential for success while optimizing the
benefit to society. The analysis utilizes a new taxonomy for organizing requirements, assesses the current gaps in spacebased
measurements and missions, assesses the impact of the current and planned space-based missions, and presents a
set of recommendations.
A compact remote Raman sensor system was developed at NASA Langley Research Center. This sensor is an
improvement over the previously reported system, which consisted of a 532 nm pulsed laser, a 4-inch telescope, a
spectrograph, and an intensified CCD camera. One of the attractive features of the previous system was its portability,
thereby making it suitable for applications such as planetary surface explorations, homeland security and defense
applications where a compact portable instrument is important. The new system was made more compact by replacing
bulky components with smaller and lighter components. The new compact system uses a smaller spectrograph
measuring 9 x 4 x 4 in. and a smaller intensified CCD camera measuring 5 in. long and 2 in. in diameter. The previous
system was used to obtain the Raman spectra of several materials that are important to defense and security applications.
Furthermore, the new compact Raman sensor system is used to obtain the Raman spectra of a diverse set of materials to
demonstrate the sensor system's potential use in the identification of unknown materials.
Recent and future explorations of Mars and lunar surfaces through rovers and landers have spawned great interest in
developing an instrument that can perform in-situ analysis of minerals on planetary surfaces. Several research groups
have anticipated that for such analysis, Raman spectroscopy is the best suited technique because it can unambiguously
provide the composition and structure of a material. A remote pulsed Raman spectroscopy system for analyzing
minerals was demonstrated at NASA Langley Research Center in collaboration with the University of Hawaii. This
system utilizes a 532 nm pulsed laser as an excitation wavelength, and a telescope with a 4-inch aperture for collecting
backscattered radiation. A spectrograph equipped with a super notch filter for attenuating Rayleigh scattering is used to
analyze the scattered signal. To form the Raman spectrum, the spectrograph utilizes a holographic transmission grating
that simultaneously disperses two spectral tracks on the detector for increased spectral range. The spectrum is recorded
on an intensified charge-coupled device (ICCD) camera system, which provides high gain to allow detection of
inherently weak Stokes lines. To evaluate the performance of the system, Raman standards such as calcite and
naphthalene are analyzed. Several sets of rock and mineral samples obtained from Ward's Natural Science are tested
using the Raman spectroscopy system. In addition, Raman spectra of combustible substances such acetone and isopropanol are also obtained.
For exploration of planetary surfaces, detection of water and ice is of great interest in supporting existence of life on other planets. Therefore, a remote Raman spectroscopy system was demonstrated at NASA Langley Research Center in collaboration with the University of Hawaii for detecting ice-water and hydrous minerals on planetary surfaces. In this study, a 532 nm pulsed laser is utilized as an excitation source to allow detection in high background radiation conditions. The Raman scattered signal is collected by a 4-inch telescope positioned in front of a spectrograph. The Raman spectrum is analyzed using a spectrograph equipped with a holographic super notch filter to eliminate Rayleigh scattering, and a holographic transmission grating that simultaneously disperses two spectral tracks onto the detector for higher spectral range. To view the spectrum, the spectrograph is coupled to an intensified charge-coupled device (ICCD), which allows detection of very weak Stokes line. The ICCD is operated in gated mode to further suppress effects from background radiation and long-lived fluorescence. The sample is placed at 5.6 m from the telescope, and the laser is mounted on the telescope in a coaxial geometry to achieve maximum performance. The system was calibrated using the spectral lines of a Neon lamp source. To evaluate the system, Raman standard samples such as calcite, naphthalene, acetone, and isopropyl alcohol were analyzed. The Raman evaluation technique was used to analyze water, ice and other hydrous minerals and results from these species are presented.
The current Earth observing capability depends primarily on spacecraft missions and ground-based networks to provide the critical on-going observations necessary for improved understanding of the Earth system. Aircraft missions play an important role in process studies but are limited to relatively short-duration flights. Suborbital observations have contributed to global environmental knowledge by providing in-depth, high-resolution observations that space-based and in-situ systems are challenged to provide; however, the limitations of aerial platforms - e.g., limited observing envelope, restrictions associated with crew safety and high cost of operations have restricted the suborbital program to a supporting role. For over a decade, it has been recognized that autonomous aerial observations could potentially be important. Advances in several technologies now enable autonomous aerial observation systems (AAOS) that can provide fundamentally new observational capability for Earth science and applications and thus lead scientists and engineers to rethink how suborbital assets can best contribute to Earth system science. Properly developed and integrated, these technologies will enable new Earth science and operational mission scenarios with long term persistence, higher-spatial and higher-temporal resolution at lower cost than space or ground based approaches. This paper presents the results of a science driven, systems oriented study of broad Earth science measurement needs. These needs identify aerial mission scenarios that complement and extend the current Earth Observing System. These aerial missions are analogous to space missions in their complexity and potential for providing significant data sets for Earth scientists. Mission classes are identified and presented based on science driven measurement needs in atmospheric, ocean and land studies. Also presented is a nominal concept of operations for an AAOS: an innovative set of suborbital assets that complements and augments current and planned space-based observing systems.
The need for better atmospheric predictions is causing the atmospheric science community to look for new ways to obtain longer, higher-resolution measurements over several diurnal cycles. The high resolution, in-situ measurements required to study many atmospheric phenomena can be achieved by an Autonomous Aerial Observation System (AAOS); however, meeting the long on-station time requirements with an aerial platform poses many challenges. Inspired by the half-scale drop test of the deployable Aerial Regional-scale Environmental Survey (ARES) Mars airplane, a study was conducted at the NASA Langley Research Center to examine the possibility of increasing on-station time by launching an airplane directly at the desired altitude. The ARES Mars airplane concept was used as a baseline for Earth atmospheric flight, and parametric analyses of fundamental configuration elements were performed to study their impact on achieving desired on-station time with this class of airplane. The concept involved lifting the aircraft from the ground to the target altitude by means of an air balloon, thereby unburdening the airplane of ascent requirements. The parameters varied in the study were aircraft wingspan, payload, fuel quantity, and propulsion system. The results show promising trends for further research into aircraft-payload design using this unconventional balloon-based launch approach.
A major concern today is to accurately measure CO2, O3, H2O, and CH4 in the atmosphere for the prediction of climate and weather. These measurements are critical for understanding the Earth's atmosphere, atmospheric chemistry, and systemic forcing driving climactic changes. For these measurements, detectors with high quantum efficiency and near background limited performance detectivity over a wide wavelength range are necessary. In this article, we will review the state-of-the-art single and multicolor detector technologies in a wide spectral-range, for use in space-based and airborne remote sensing applications. Simultaneous detection in multi-wavelength bands with a single focal plane array (FPA) will result in reduction or elimination of heavy and complex optical components now required for wavelength differentiation in atmospheric remote sensors leading to smaller, lighter, simpler instruments with higher performance. Discussions are focused on current and the most recently developed FPA in addition to emphasizing future development in UV-to-Far infrared multicolor FPA detectors for next generation space-based instruments to measure water vapor and greenhouse gases. This novel detector component will make instruments designed for these critical measurements more efficient while reducing complexity and associated electronics and weight. Finally, we will discuss the on-going detector technology efforts at NASA Langley Research Center (LaRC), Jet Propulsion Laboratory (JPL), and Rensselaer Polytechnic Institute (RPI).
KEYWORDS: Sensors, Avalanche photodetectors, Information operations, LIDAR, Receivers, Signal to noise ratio, Telescopes, Signal detection, Analog electronics, Optical design
NASA Langley has an active water vapor differential absorption lidar program taking measurements from both C-130 and ER-2 aircraft. A research effort has started to increase the signal-to-noise ratio in the DIAL receiver by 1) evaluating new very low noise avalanche photo didoes (APD), 2) designing an optics system that will focus the return light signal to the APD efficiently and 3) constructing a 10-MHz waveform digitizer board that will be small enough to be placed at the APD and telescope. With these advances we anticipate improving the signal-to-noise ratio by a factor of ten over the current receiver system.
NASA Langley Research Center (LaRC) is sponsoring the development of a revolutionary new concept for remote sensing from space. This concept is based on new technology and differs radically from previous paradigms, which call for building instruments that bolt to spacecraft. Langley's concept is called a 'sensorcraft.' The term sensorcraft simply designates a spaceflight remote sensing system that does not distinguish between the instrument, which performs a remote measurement, and the spacecraft bus, which provides the operational resources needed by the instrument in orbit. It integrates the resource requirements of both to minimize size, power consumption and cost. The gas and aerosol monitoring sensorcraft (GAMS) is a technology development project that seeks to revolutionize the remote sensing technique of solar occultation. An inherent limitation of solar occultation is the spatial and temporal coverage from a single spacecraft. For any given orbit there are at most two opportunities to take data, one at sunrise and one at sunset. A single satellite takes months to obtain a sufficient number of events to achieve global coverage. One solution to quicker global coverage is to launch several copies of the satellite. Unfortunately, by today's standards, this is very costly in hardware, launch costs, and in mission operations. This paper describes the effort to produce a small, inexpensive satellite that requires minimal ground support effort. Such a satellite would be cost effective to mass-produce, be a good 'payload of opportunity,' and allow for a constellation approach yielding global coverage in a matter of days. The GAMS project will produce an autonomous sensorcraft with mass of 60 kg, requiring less than 50 W average power and costing less than $2 M. GAMS will also perform extensive onboard processing which not only helps to reduce size and weight, but will minimize mission operations requirements. A validation flight is targeted for Shuttle deployment in late 1999. This paper discusses the mission concept and the key technologies GAMS will employ to achieve a tenfold decrease in science mission costs.
Space-based observation of tropospheric pollution has been identified as an important measurement to be included in Earth science missions of the 21st century. This presentation will summarize on-going efforts focused on enabling such a new capability, a high-priority atmospheric science mission for the measurement of tropospheric ozone from a space-based platform, through the implementation of Fabry-Perot interferometry. The measurement technique involves a double-etalon series configuration FPI along with an ultra-narrow bandpass filter to achieve single-order operation with an overall spectral resolution of approximately .068 cm-1, sampling a narrow spectral region within the strong 9.6 micrometers ozone infrared band form a nadir-viewing satellite configuration. Current research efforts are focusing on technology development and demonstration activities to address technology drivers associated with this measurement concept. To this end we have developed a small-scale, modular, double-etalon prototype FPI for laboratory characterization and testing, modelled the instrument optical configuration, and performed R and D associated with an etalon optical control scheme. This presentation will cover advancements pertaining to all aspects of this effort, however, emphasis will be placed on integration and testing activities associated with the laboratory prototype FPI. This will include multichannel operation considerations pertaining to different configurations for spectral tuning. In addition, implications associated with extrapolation toward a full- scale flight instrument design will also be addressed.
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