To meet Naval needs for sensing of the global environment, the Office of Naval Research (ONR) and the Naval Research Laboratory (NRL) sponsor or carry out a variety of research programs using hyperspectral sensing. For ocean sensing, airborne and space-borne hyperspectral sensors are used to characterize the littoral environment with the aim of providing specification of ocean optical parameters including water clarity, diver visibility, bathymetry, bottom type and beach characterization. For the atmosphere, the Navy has interest in hyperspectral remote sensing from geosynchronous orbit. ONR interests include improved modeling of radiation transport in the atmosphere to infer high resolution profiles of wind, temperature and minor species and cloud characteristics. With sponsorship from Director Defense Research and Engineering (DDR&E), ONR is managing a Multidisciplinary University Research Initiative (MURI) to provide new models for use with geosynchronous data. In partnership with NASA, NOAA and the Air Force, ONR is promoting the flight of the Geosynchronous Imaging Fourier Transform Spectrometer-Indian Ocean METOC Imager (GIFTS-IOMI) program to obtain hyperspectral atmospheric imagery with high spatial, spectral and temporal resolution. For the space environment, NRL has flown a suite of experimental ultraviolet hyperspectral sensors to determine altitude profiles of the ionospheric electron density and upper atmospheric neutral density. The High Resolution Airglow/Aurora Spectroscopy (HIRAAS) experiment on the ARGOS satellite provided a proof of concept for a future series of hyperspectral ultraviolet space weather sensors the first of which has recently been launch on a DMSP weather satellite. ONR is sponsoring the development of a multispectral ultraviolet imager to take this capability to geosynchronous orbit.
Traditionally the ionosphere and thermosphere are considered "data-starved" regions of the atmosphere but recent experimental and operational optical satellite instruments and new techniques to exploit GPS and orbiting radio beacons are dramatically improving the situation. Similarly, new classes of assimilating ionospheric models are under development to exploit these data and provide a significantly improved capability to specify and forecast weather of the upper atmosphere and ionosphere. The Advanced Research and Global Observation Satellite (ARGOS), launched by the DoD Space Test Program in 1999 demonstrated ultraviolet remote sensing of the neutral atmosphere and ionosphere from limb sensors in low Earth orbit (LEO). Soon after, the Global Ultraviolet Imager (GUVI) on the NASA TIMED satellite employed a similar capability using cross track ultraviolet remote sensing. The first of five sets of operational versions of both of these instruments, the Special Sensor Ultraviolet Limb Imager (SSULI) and Special Sensor Ultraviolet Spectroscopic Imager (SSUSI), respectively, where launched aboard the first of the DMSP Block 5D3 weather satellites in October of 2003. Radio frequency techniques for ionospheric remote sensing using ground-based dual frequency GPS receivers and GPS occultation receivers on LEO satellites are making a significant contribution to the global ionospheric database. In 2005, the launch of a constellation of six satellites called the Constellation Observing System for Meteorology, Ionosphere and Climate (COSMIC) will provide ionospheric measurements using GPS occultation receivers ultraviolet photometers and dual frequency UHF radio beacons. The latter will allow tomographic ionospheric reconstructions using ground-based receivers. These and other data will be used to drive the Global Assimilations of Ionospheric Measurements (GAIM) model to dramatically improved current modeling and forecast capabilities for the global thermosphere and ionosphere. More innovations are under development in the form of long-dwell, high temporal and spatial resolution measurements of the ionosphere from geosynchronous orbit using the Ionospheric Mapping and Geocoronal Experiment (IMAGER). IMAGER will provide GOES-like monitoring of the ionosphere and neutral atmosphere.
We present the concept for an instrument designed to map and monitor the ionosphere from geostationary orbit. This instrument will be used to study the spatial and temporal behavior of mesoscale (> 10 km) ionospheric structures. The instrument is designed to primarily operate at night as irregularities are generally more prevalent during the evening. The instrument will be sensitive enough to gather a high signal-to-noise image viewing the nadir in approximately 100 seconds. The instrument can also be operated as a limb imager. The instrument will image a 1.6 degree(s) field-of-view with 10 km spatial resolution. The experiment will use a two-axis gimbal to point to various points on the limb and disk of the Earth. The instrument consists of an extreme ultraviolet (EUV) imager and a far-ultraviolet (FUV) imager. The EUV imager will operate at 83.4 nm using a low resolution imaging spectrograph to set the passband. The O II 83.4 nm emission is produced by photoionization of O during the daytime. Above the limb, this emission can be used to determine altitude distribution of the O+ density. The FUV imager will operate at 130.4 , 135.6, and 143.0 nm. At night, The O I 130.4 and O I 135.6 nm emissions are produced by primarily by radiative recombination, and therefore these emissions provide useful ionospheric diagnostics at night. During the daytime, the 130.4 and 135.6 nm lines are primarily produced by photoelectron impact excitation of O; however the 130.4 nm line is also excited by resonant scattering of sunlight. The O I 130.4 and 135.6 nm lines provide information on the O density during the daytime. The instrument will map the daytime N2 column density using the Lyman-Birge-Hopfield bands near 143.0 nm.
The Advanced Research and Global Observation Satellite (ARGOS) has been operating since February 1999 and includes three spectrographs comprising the High Resolution Airglow and Auroral Spectroscopy (HIRAAS) experiment. The HIRAAS instruments remotely sense the Earth's mid-, far- and extreme-ultraviolet airglow to study the density, composition, and temperature of the thermosphere and ionosphere. The Low Resolution Airglow and Aurora Spectrograph (LORAAS) is a limb scanner covering the 80-170 passband nm with 1.8 nm spectral resolution. Repeated serendipitous observations of hot O- and B-type stars have been used to improve the aspect solution, characterize the instrument field-of-view, and monitor relative sensitivity degradation of the instrument during the mission. We present the methodology of performance characterization and report the observed performance degradation of the LORAAS wedge-and-strip microchannel plate detector. The methods and results herein can be utilized directly in on-orbit characterization of the SSULI operational sensors to fly aboard the DMSP Block 5D3 satellites.
The High-resolution Ionospheric and Thermospheric Spectrograph (HITS) is a very high resolution (> 0.5 angstroms resolution over the 500 - 1500 angstroms passband) Rowland circle spectrograph that is currently flying on the USAF Advanced Research and Global Observing Satellite (ARGOS, launched 23 February 1999). The ARGOS is in a sun- synchronous, near-polar orbit at 833 km altitude with an ascending node crossing time of 2:30 PM. The instrument is designed to spectrally resolve the 834 angstroms triplet to demonstrate a new technique for remotely sensing the electron density in the F-region ionosphere. In addition, the HITS can spectrally resolve the rotational structure of the N2 Lyman-Birge-Hopfield bands, which can be used to infer the thermospheric temperature. The HITS can resolve the radiative recombination continuum produced by recombining O+ ions and electrons, which can be used to infer the electron temperature. The HITS will also produce a high spectral resolution array of the 500 - 1000 angstroms passband to produce a more accurate identification of some of the previously unresolved features of the dayglow spectrum. The instrument operates as a limb imager with a limb scan occurring every 100 seconds throughout the expected three year mission life. Its field-of-view is 0.06 degree(s) X 4.6 degree(s), which corresponds to 3 km (altitude) X 230 km (along the horizon) at the limb. The instrument's field-of-regard is 17 degree(s) X 4.6 degree(s), which covers the 100 - 750 km altitude range. We will present an overview of the instrument and discuss its calibration and in-flight performance.
The High Resolution Airglow and Aurora Spectrograph flew on sounding rockets in 1990, 1992, and 1994. The instrument obtained over 300 exposures (600 spectra) varying in length from 0.3 seconds to 10 seconds during the three flights. The first two flights observed the UV dayglow above the White Sands Missile Range, Las Cruces, NM. The instrument was flown a third time from the Poker Flat Research Range, Fairbanks, AK where it observed a proton aurora. We will present an overview of the instrument and discuss its calibration and its performance during the three flights.
The Ionospheric Spectroscopy And Atmospheric Chemistry Experiment is a high resolution mid-ultraviolet Ebert-Fastie spectrograph that is flying on the USAF Advanced Research and Global Observing Satellite (ARGOS, launched 23 February 1999). The instrument is designed to spectrally resolve the rotational structure of the nitric oxide bands, which will be used to infer the temperature in the lower thermosphere (90 - 200 km altitude range). The instrument is operated as a limb imager with a limb scan occurring every 100 seconds throughout the expected three year mission life. The ARGOS is in a sun-synchronous, near-polar orbit at 833 km altitude with an ascending node crossing time of 2:30 PM. We will present an overview of the instrument and discuss its calibration and in-flight performance.
The Special Sensor Ultraviolet Limb Imager (SSULI) program involves the development of a series of five ultraviolet limb imaging spectrographs by the Naval Research Laboratory for the Defense Meteorological Satellite Program. In addition, a duplicate sixth instrument, the Low Resolution Airglow/Aurora Spectrograph (LORAAS) will be flown aboard the Space Test Program ARGOS satellite in late 1997. These instruments will measure vertical intensity profiles of the Earth's airglow in the extreme and far ultraviolet (800 to 1700 angstroms) with 19 angstroms resolution. The instruments view the limb using a rotating mirror to scan the 0.1 degree(s) X 2.4 degree(s) field of view from 750 km to 50 km tangent altitude. SSULI measurements will be used to infer altitude profiles of ion, electron and neutral density. The first SSULI is scheduled to launch in 2000, and coverage from all the instruments will provide a continuous atmospheric data set spanning an entire solar cycle. The first four SSULI instruments are complete, and detailed optical calibrations have been performed. Assembly and calibration of the remaining SSULI instrument and LORAAS are underway, and preliminary results are available. Preliminary results of the first SSULI instrument were reported in 1994. This paper updates the calibration results of the first instrument and presents a summary of the results of the next three SSULI instruments. Comparison between instrument characteristics are also discussed, including variations in calibration techniques. A brief discussion on the periodic calibration verification of the SSULI instruments during storage and prior to launch is included.
Over the next five years the Naval Research Laboratory (NRL) will fly a series of ultraviolet satellite instrument packages to measure vertical profiles of atmospheric airglow emission. The objective of this program is to test new techniques for optical remote sensing of the mesosphere, thermosphere, and ionosphere using limb scanning spectrographs. Emphasis will be placed on day- and night-remote sensing of the F-region through measurement of profiles of airglow emission from the O+ ion. Other objectives include remote sensing of vertical profiles of neutral density, minor species and temperature. These observations will be used to study the composition, photochemistry, thermodynamics, and couplings between atmospheric regions. A phased approach will be used which provides for: (1) comprehensive multi-parameter measurements; (2) high spectral resolution studies; and (3) long-term operational observations from DoD weather satellites. The first of these payloads is the multi- sensor experiment called the remote atmospheric & ionospheric detection (RAIDS). RAIDS, a collaboration between NRL and The Aerospace Corporation, contains two spectrographs, three scanning grating spectrometers, and three photometers. Space flight for RAIDS will be provided by the Air Force Space Test Program (STP). The phase 2 component is the high resolution airglow/aurora spectroscopy (HIRAAS) experiment, a collaboration between NRL and the Naval Postgraduate School. HIRAAS will fly aboard the STP ARGOS Satellite in early 1996. The third phase of this program involves flight of a series of five limb scanning instruments called the special sensor ultraviolet limb imager (SSULI) aboard Defense Meteorological Satellite Program weather satellites in the last quarter of this decade. The long- term observations from these satellite experiments will provide a comprehensive database of mesospheric, thermospheric, and ionospheric density profiles from which to search for the effects of global change.
The special sensor ultraviolet limb imager (SSULI) is an ultraviolet limb imaging spectrograph under development by the Naval Research Laboratory for the Defense Meteorological Satellite Program (DMSP). The instrument will measure limb intensity profiles of the earth's airglow in the extreme and far ultraviolet (800 to 1700 angstrom) with 12 - 15 angstrom resolution. The SSULI uses a rotating mirror to scan the instrument field-of-view through 17 degrees to view from 750 km to 50 km tangent altitude. SSULI measurements will be used to infer altitude profiles of ion and electron density and neutral density. A total of five SSULI instruments will be flown on the DMSP Block 5D3 satellites the first of which is scheduled for launch in the latter half of the decade. An additional copy will be flown aboard the Space Test Program (STP) ARGOS satellite in late 1995. Every optical component in SSULI was independently measured followed by system level instrument calibrations. The first SSULI instrument is complete and the preliminary calibration results validate the design expectations. Assembly and calibration of the remaining instruments is underway. This paper presents the preliminary calibration results from SSULI #1 and component test results of the wedge and strip anode microchannel plate detector, grating, collimator and scan mirror. In addition, calibration techniques used to determine detector quantum efficiency, counting linearity, resolution, wavelength and absolute calibration are discussed. A brief discussion of the log term calibration plans for the SSULI instruments including periodic calibration checks during storage, in-flight calibrations using stars and ground truth measurements is presented.
A facility for calibrating far ultraviolet and extreme ultraviolet instruments has recently been completed at the Naval Research Laboratory. Our vacuum calibration vessel is 2-m in length, 1.67-m in diameter, and can accommodate optical test benches up to 1.2-m wide by 1.5-m in length. A kinematically positioned frame with four axis precision pointing capability of 10 microns for linear translation and .01 degrees for rotation is presently used during vacuum optical calibration of SSULI. The chamber was fabricated from 304 stainless steel and polished internally to reduce surface outgassing. A dust-free environment is maintained at the rear of the vacuum chamber by enclosing the 2-m hinged vacuum access door in an 8 ft. by 8 ft. class 100 clean room. Every effort was made to obtain an oil-free environment within the vacuum vessel. Outgassing products are continually monitored with a 1 - 200 amu residual gas analyzer. An oil-free claw and vane pump evacuates the chamber to 10-2 torr through 4 in. diameter stainless steel roughing lines. High vacuum is achieved and maintained with a magnetically levitated 480 l/s turbo pump and a 3000 l/s He4 cryopump. Either of two vacuum monochrometers, a 1-m f/10.4 or a 0.2-m f/4.5 are coaxially aligned with the optical axis of the chamber and are used to select single UV atomic resonance lines from a windowless capillary or penning discharge UV light source. A calibrated channeltron detector is coaxially mounted with the SSULI detector during calibration. All vacuum valves, the cooling system for the cryopump compressor, and the roughing pump are controlled through optical fibers which are interfaced to a computer through a VME board. Optical fibers were chosen to ensure that complete electrical isolation is maintained between the computer and the vacuum system valves-solenoids and relays.
The Naval Research Laboratory is developing a series of far- and extreme-ultraviolet spectrographs (800 to 1700 Å) to measure altitude profiles of the ionospheric and thermospheric airglow from the U.S. Air Force Defense Meteorological Satellite Program's Block 5D3 satellites. These spectrographs, which comprise the Special Sensor Ultraviolet Limb Imager (SSULI), use a near-Wadsworth optical configuration with a mechanical grid collimator, concave grating, and linear array detector. To image the limb, SSULI employs a rotating planar SiC mirror that sweeps the field of view perpendicular to the limb of the Earth. In the primary operating mode, the mirror sweeps the instrument field of view through 17 deg to view tangent heights from about 50 to 750 km. The SSULI detectors use microchannel plate intensification and wedge-and-strip decoding anodes to resolve 256 pixels in wavelength dispersion. The detector is windowless and uses an o-ring sealed door to protect the Csl photocathode from exposure prior to insertion in orbit. The altitude distributions of the airglow measured by the SSULI sensors will be used to infer the altitude distributions of electrons and neutral species. At night, electron densities will be determined by measurement of ion recombination nightglow. Daytime electron densities will be obtained from measurements of multiple resonant scattering of O+ 834-Å radiation produced primarily by photoionization excitation of atomic oxygen. Dayside neutral densities and temperatures will be inferred from the measurement of dayglow emissions from N2 and O produced by photoelectron impact excitation.
Robert McCoy, Robert Meier, Kenneth Wolfram, J. Picone, Stefan Thonnard, Gilbert Fritz, Jeff Morrill, David Hardin, Andrew Christensen, David Kayser, James Pranke, Paul Straus
The Remote Atmospheric and Ionospheric Detection System (RAIDS) experiment is an optical remote sensing platform consisting of eight sensors, (spectrographs, spectrometers, and photometers) covering the wavelength range 550 to 8744 Å. RAIDS employs a mechanical scan platform to view the Earth's limb and measure line-of-sight column emission from tangent altitudes from 50 to 750 km. These measurements provide vertical profiles of atmospheric dayglow and nightglow from the mesosphere to the upper regions of the F-region ionosphere. RAIDS will be flown on the National Oceanographic and Atmospheric Administration (NOAA) J weather satellite through the auspices of the U.S. Air Force Space Test Program. The RAIDS wavelength and altitude coverage allows remote sensing of the major and many minor constituents in the thermosphere and ionosphere. These measurements will be used as part of a proof of concept for remote sensing of ionospheric and neutral density profiles. The RAIDS database will be used to study composition, thermal structure, and couplings between the mesosphere, thermosphere, and ionosphere. RAIDS is a joint venture of the Naval Research Laboratory (NRL) and The Aerospace Corporation. We describe the subset of RAIDS instruments developed at NRL covering the far to near UV regions (1300 to 4000 Å).
Andrew Christensen, David Kayser, James Pranke, Paul Straus, David Gutierrez, Supriya Chakrabarti, Robert McCoy, Robert Meier, Kenneth Wolfram, J. Picone
The Remote Atmospheric and Ionospheric Detection System experiment consists of eight instruments spanning the wavelength range from the extreme ultraviolet (55 nm) to the near infrared (800 nm) oriented to view the Earth's limb from the National Oceanic and Atmospheric Administration TIROS-J spacecraft to be launched into a circular orbit in 1993. Through measurements of the natural optical emissions and scattered sunlight originating in the upper atmosphere including the mesosphere and thermosphere, state variables such as temperature,
composition, density, and ion concentration of this region will be inferred. The subset of instruments fabricated or otherwise provided by the Space and Environment Technology Center (formerly Space Sciences Laboratory) at The Aerospace Corporation are described.
The Naval Research Laboratory (NRL) has been developing far- and extreme-ultraviolet spectrographs for remote sensing the Earth's upper atmosphere and ionosphere. The first of these sensors, called the Special Sensor Ultraviolet Limb Imager (SSULI), will be flying on the Air Force's Defense Meteorological Satellite Program (DMSP) block 5D3 satellites as an operational sensor in the 1997-2010 time frame. A second sensor, called the High-resolution Ionospheric and Thermospheric Spectrograph (HITS), will fly in late 1995 on the Air Force Space Test Program's Advanced Research and Global Observation Satellite (ARGOS, also known as P91-1) as part of NRL's High Resolution Airglow and Auroral spectroscopy (HIRAAS) experiment. Both of these instruments are compact and do not draw much power and would be good candidates for small satellite applications. The instruments and their capabilities are discussed. Possible uses of these instruments in small satellite applications are also presented.
Chemical vapor deposited (CVD) silicon carbide mirrors were exposed to bombardment by 8 km/s (5.2 eV) oxygen atoms that simulated exposure in low earth orbit for periods up to 7.5 years. The reflectances of four mirrors were measured before and after exposure at 584, 736, 1048, 1216, and 1610 angstroms and at eleven angles of incidence ranging from 5 degree(s) to 80 degree(s). The oxygen exposure reduced the normal incidence reflectances by factors of 1.5 to 4.5 in the VUV but had no effect on the visual appearance. The optical constants and thicknesses of the surface layers present on the SiC substrates were determined from reflectance measurements. This analysis indicated that before exposure the surface layers were composed of SiOx (where x approximately equals 1.5) with thicknesses of 8 - 18 angstroms. After exposure the thicknesses had increased to 35 - 45 angstrom. There were no systematic differences in the reflectances after simulated space exposures of 1.5, 4.5, and 7.5 years. This implied that most of the growth in thickness of the SiOx layers occurred early in the exposure and stabilized at thicknesses of 35 - 45 angstroms. The optical results were consistent with x-ray photoelectron spectroscopy of the four mirrors after oxygen exposure.
Robert McCoy, Robert Meier, Kenneth Wolfram, J. Picone, Stefan Thonnard, Gilbert Fritz, Jeff Morrill, David Hardin, Andrew Christensen, David Kayser, James Pranke, Paul Straus
The RAIDS experiment is an optical remote sensing platform consisting of eight sensors (spectrographs, spectrometers and photometers) covering the wavelength range 550 A to 8744 A. RAIDS employs a mechanical scan platform to view the Earth's limb and measure vertical profiles of atmospheric dayglow and nightglow from the mesosphere to the upper regions of the F region ionosphere (75 -750 km). RAIDS will be flown on the NOAA J weather satellite through the auspices of the Air Force Space Test Program (STP). The RAIDS wavelength and altitude coverage allows remote sensing of the major, and many minor constituents in the thermosphere and ionosphere. These measurements will be used as part of a proof-of-concept for remote sensing of ionospheric and neutral density profiles. The RAIDS database will be used to study composition, thermal structure and couplings between the mesosphere, thermosphere and ionosphere. RAIDS is a joint venture of the Naval Research Laboratory (NRL) and The Aerospace Corporation. This paper describes the subset of RAIDS instruments developed at NRL covering the far to near ultraviolet (1300 A - 4000 A). A companion paper describes the balance of the experiment complement.
Andrew Christensen, David Kayser, James Pranke, Paul Straus, David Gutierrez, Supriya Chakrabarti, Robert McCoy, Robert Meier, Kenneth Wolfram, J. Picone
The RAIDS experiment consists of eight instruments spanning the wavelength range from the extreme ultraviolet (55 nm) to the near infrared (800 nm) oriented to view the Earth's limb from the NOAA-J spacecraft to be launched into a circular orbit in 1993. Through measurements of the natural optical emissions and scattered sunlight origmating in the upper atmosphere including the mesosphere and thermosphere, state variables such as temperature, composition, density and ion concentration of this region will be inferred. This paper describes the subset of instruments fabricated or otherwise provided by the Space and Environment Technology Center (formerly Space Sciences Laboratory) at The Aerospace Corp. The companion to this paper describes the instruments from the Naval Research Laboratory. The Extreme Ultraviolet Spectrograph (EUVS), the three fixed filter photometers 0! (630), 0! (777), and Na (589), and the near infrared spectrometer (NIR) will be described. These are all mounted on a mechanical scan platform that scans the limb from approximately 75 to 750 km in the orbital plane of the satellite every 90 seconds.
The Naval Research Laboratory is developing a limb imaging far- and extreme-ultraviolet (FUV/EUV) spectrograph (800-1700 A) to measure vertical profiles of the ionospheric and thermospheric airglow from DMSP Block 5D3 satellites. The spectrograph, called the Special Sensor Ultraviolet Limb Imager (SSULI), uses a near-Wadsworth optical configuration with a mechanical grid collimator, concave grating and linear array detector. Measured airglow profiles from the SSULI sensors will be used to infer vertical profiles of electron density and neutral density. At night, electron densities will be determined by measurement of ion recombination nightglow. Daytime electron densities will be obtained from measurements of multiple resonant scattering of O(+) 834 A radiation produced primarily by photoionization excitation. Dayside neutral densities and temperatures will be inferred from measurement of dayglow emissions from N2 and O produced by photoelectron impact excitation.
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