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Cubesat Constellation Design for Air Traffic Monitoring
Suitably equipped global and local air traffic can be tracked. The tracking information may then be used for control from ground-based stations by receiving the Automatic Dependent Surveillance-Broadcast (ADS-B) signal. The ADS-B signal, emitted from the aircraft's Mode-S transponder, is currently tracked by terrestrial based receivers but not over remote oceans or sparsely populated regions such as Alaska or the Pacific Ocean. Lack of real-time aircraft time/location information in remote areas significantly hinders optimal planning and control because bigger "safety bubbles" (lateral and vertical separation) are required around the aircraft until they reach radar-controlled airspace. Moreover, it presents a search-and-rescue bottleneck. Aircraft in distress, e.g. Air France AF449 that crashed in 2009, take days to be located or cannot be located at all, e.g. Malaysia Airlines MH370 in 2014. In this paper, we describe a tool for designing a constellation of small satellites which demonstrates, through high-fidelity modeling based on simulated air traffic data, the value of space-based ADS-B monitoring and provides recommendations for cost-efficient deployment of a constellation of small satellites to increase safety and situational awareness in the currently poorly-served surveillance area of Alaska. Air traffic data has been obtained from the Future ATM Concepts Evaluation Tool (FACET), developed at NASA Ames Research Center, simulated over the Alaskan airspace over a period of one day. The simulation is driven by MATLAB with satellites propagated and coverage calculated using AGI's Satellite ToolKit(STK10).
A Review of NASA Ames CubeSat Program
This is a brief overview of NASA Ames' work in small Satellites.
CubeQuest Challenge: Advanced CubeSat Technologies for Affordable Deep Space Science and Exploration Missions
No abstract available
Thermal Assessment of Paraffin Phase Change Material Mini-Packs on IceCube 3U CubeSat in Flight
Three paraffin phase change material (PCM) mini-packs were flown on the IceCube instrument in the International Space Station (ISS) orbit. They contained a total of 40.69 g of n-Hexadecane. In flight, from Day of Year (DOY) 250-255 in 2017, the IceCube instrument operation scheme was "Day-On Every Other Orbit." The instrument power-on time was approximately 45.6 minutes longer than the design power-on time. Its power-off time was 47 minutes longer than the design power-off time. Flight temperature telemetry data revealed that latent heat change of the paraffin PCM maintained the instrument temperatures at about 18 degrees Centigrade most of the time. It validated the functionality of the paraffin PCM mini-packs.
A CubeSat-Payload Radiation-Reliability Assurance Case Using Goal Structuring Notation
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The Lunar Flashlight Propulsion System - A Green Chemical Propulsion System for CubeSats
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Achieving Game-Changing Science with Cubesats adn SmallSats
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Achieving Game-Changing Science with CubeSats and SmallSats
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Achieving Game-Changing Science with CubeSats and SmallSats
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Lessons Learned Developing Flight, Ground, and Mission Operations Software for the GPX2 Technology Demonstration 3U CubeSat
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Tsunami Early-Warning CubeSat Design Reference Mission (DRM)
Global constellation for near real-time detection, characterization, and warning of dangerous tsunami; detection and evaluation of large earthquakes and volcanic eruptions; and study and continuous monitoring of the ionosphere and climate change.
TBIRD, A Rapid Prototyping Approach for Design, Assembly, and Test of A LEO-to-Ground Lasercom Cubesat
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Starling CubeSat Swarm: Flight Results and Lessons Learned
A review of lessons learned from the NASA Starling primary mission.
Development and On-Orbit Operation of the NACHOS CubeSat-Based Trace-Gas Hyperspectral Imager
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Optical calibration and first light for the deformable mirror demonstration mission CubeSat (DeMi)
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