National Aeronautics and Space Administration
Small Business Innovation Research & Technology Transfer 2003 Program Solicitations

TOPIC T4 Goddard Space Flight Center

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T4.01 Astronomy, Physics and Earth Sciences



T4.01 Astronomy, Physics and Earth Sciences

The mission of the Earth Science Enterprise is to develop a scientific understanding of the Earth system and its responses to natural and human-induced changes to enable improved prediction of climate, weather, and natural hazards for present and future generations. By leveraging breakthrough technologies from terrestrial applications, as well as the vantage point of space, we seek to observe, analyze, and model the Earth system to discover how it is changing and the consequences for life on Earth.

The mission of the Space Science Program is to solve mysteries of the universe, explore the solar system, discover planets around other stars, search for life beyond Earth, chart the evolution of the universe and understand its galaxies, stars, planets, and life. The Space Science Program seeks to understand the universe from the beginning of time, looking ever deeper with increasingly more capable telescopes to scan the entire electromagnetic spectrum from gamma rays to radio wavelengths.

This STTR solicitation is to help provide advanced remote sensing technologies to enable future Earth and Space Science measurements.

Analytical Instrumentation for Planetary Atmospheres Research
Innovations and the application of new technologies are sought for improving the operating characteristics of gas chromatograph-mass spectrometer systems in harsh environments. Reductions in volume, weight, power and cost while increases in performance, serviceable, functionality of system components is highly desirable. The overall goal is to develop an instrument with increased performance in the areas of improved collection, detection and measurement. Specific area of interest include:


Active Optical Systems and Technology for UAVs and Ballooncraft
Lidar remote sensing systems are required to meet the demanding requirements for future Earth Science missions. It is envisioned that lidar systems will be used in the following application areas: high spatial and temporal resolution observations of the land surface and vegetation cover (biomass); profiling of clouds, aerosols and atmospheric state variables including temperature, humidity, winds and trace constituents including tropospheric and stratospheric ozone and CO2 (profiling and total column); measurement of the air/sea interface and mixed layer. New systems and approaches are sought in these areas, which will:


Systems and approaches will be considered which demonstrate a capability that is scalable to space or can be mounted on a relevant platform (UAV, long duration balloon, or aircraft) for calibration/validation of a spaceborne system.

Ballooncraft Remote Sensing Detector Systems and Components
Innovative developments are being sought that incorporate new architectures, new technologies and advanced remote sensing techniques to make space science measurements. It is anticipated that these new sensors will be flown aboard spaceflight of balloon-borne platforms, and therefore emphasis on low weight, small volume and low power is very important. The innovations sought include:


Ballooncraft Trajectory Control and Station-Keeping
Trajectory Control and Station-Keeping are critical items for future Ultra Long Duration Balloon remote sensing concepts.


Unmanned Aerial Vehicle (UAV) Technologies for Remote Sensing
Avionics, real-time telemetry acquisition and remote sensing spectral imaging devices to support Unmanned Aerial Vehicles' (UAV) basic and applied science and application demonstrations (offerors need only to respond to a minimum of one of the below):


Microwave measurements using large aperture systems
New breakthrough technologies are sought for the construction of extremely large (tens of meters and larger diameter) microwave antenna systems. The systems must be compact upon launch, they must achieve high precision surface form factors, and they must include beam-scanning capabilities. The antenna compactness on launch can be achieved either through folding technologies or from some assemblage of small components into the larger final system in space. The microwave antenna surface characteristics must be accurate enough to produce microwave beam patterns with adequately small side lobes. The beam scanning must be facile and over many beam widths so as to enable cross-track scanning if in LEO, or scanning over the full globe if at GEO. The beam widths must be small enough to resolve the few kilometer scales needed for many geophysical observations. The microwave wavelengths will be determined according to the geophysical measurement of interest. The antenna concepts may include large single apertures or apertures composed of multiple elements that are operated synergistically so as to product the desired performance.


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