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  • Other Sources  (4)
  • Spacecraft Design, Testing and Performance  (4)
  • 2015-2019  (3)
  • 1990-1994  (1)
  • 1980-1984
  • 1
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    Edison Demonstration of Smallsat Networks (2015)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: The goal of NASA's Edison Demonstration of Smallsat Networks (EDSN) mission is to demonstrate interactive satellite swarms capable of collecting, exchanging and transmitting multi-point scientific measurements. Satellite swarms enable a wide array of scientific, commercial and academic research not achievable with a single satellite. The EDSN satellites are scheduled to be launched into space as secondary payloads on the first flight of the Super Strypi launch vehicle no earlier than Oct. 29, 2015.
    Keywords: Spacecraft Design, Testing and Performance
    Type: NASA FS-2015-03-01-ARC , ARC-E-DAA-TN25949
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Cubesat Proximity Operations Demonstration (CPOD) (2015)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: The CubeSat Proximity Operations Demonstration (CPOD) project will demonstrate rendezvous, proximity operations and docking (RPOD) using two 3-unit (3U) CubeSats. Each CubeSat is a satellite with the dimensions 4 inches x 4 inches x 13 inches (10 centimeters x 10 centimeters x 33 centimeters) and weighing approximately 11 pounds (5 kilograms). This flight demonstration will validate and characterize many new miniature low-power proximity operations technologies applicable to future missions. This mission will advance the state of the art in nanosatellite attitude determination,navigation and control systems, in addition to demonstrating relative navigation capabilities.The two CPOD satellites are scheduled to be launched together to low-Earth orbit no earlier than Dec. 1, 2015.
    Keywords: Spacecraft Design, Testing and Performance
    Type: CPOD-FS-2015-03-19-ARC , ARC-E-DAA-TN25951 , Small Satellite Conference; Aug 08, 2015 - Aug 13, 2015; Logan, UT; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    SmallSat Precision Navigation with Low-Cost MEMS IMU Swarms (2015)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: The continued advancement of small satellite-based science missions requires the solution to a number of important technical challenges. Of particular note is that small satellite missions are characterized by tight constraints on cost, mass, power, and volume that make them unable to fly the high-quality Inertial Measurement Units (IMUs) required for orbital missions demanding precise orientation and positioning. Instead, small satellite missions typically fly low-cost Micro-Electro-Mechanical System (MEMS) IMUs. Unfortunately, the performance characteristics of these MEMS IMUs make them ineffectual in many spaceflight applications when employed in a single IMU system configuration.
    Keywords: Spacecraft Design, Testing and Performance
    Type: NASA FS-2015-03-27-ARC , ARC-E-DAA-TN25937 , Annual AIAA/USU Conference on Small Satellite; Aug 08, 2015 - Aug 13, 2015; Logan, UT; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    COMET progresses toward first mission (1992)
    In:  CASI
    Details
    Publication Date: 2019-08-16
    Description: The Commercial Experiment Transporter (COMET) is a set of hardware and related infrastructure used to support orbital experiments of the CCDS's and their industrial partners. During this year major support contracts were signed, preliminary design reviews conducted, experiments selected for the first mission, and long lead items placed on order. The Program Office and CCDS Monitors took an active role in guiding COMET through the activation maze. Launch and recovery sites were selected and licenses for the launch vehicle, recovery system, and recovery operations were filed by the contractors with the Department of Transportation. As the period closed, COMET was preparing for Critical Design Reviews on all major systems and a target launch date was selected. This report deals primarily with the programmatic issues which were resolved as the program matured. At times it is impossible to disassociate the technical from the programmatic and, in such cases the technical material is presented to provide insight into the paths selected by both CCDS and Contractor Management.
    Keywords: Spacecraft Design, Testing and Performance
    Type: CSTAR 3rd Annual Technical Symposium Proceedings; 113-121; NASA-CR-199702
    Format: text
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    NASA TECHNICAL REPORTS
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