Engineering topics
Swenson, Charles
Publications and source records attributed to Swenson, Charles.
The Active Thermal Architecture: Thermal Control for Small-Satellites: SSC21-S1-52
No abstract provided
CubeSat Active Thermal Control in Support of Advanced Payloads: The Active Thermal Architecture
No abstract provided
CubeSat Active Thermal Control in Support of Advanced Payloads: The Active Thermal Architecture Project
The Active Thermal Architecture (ATA) is an advanced sub-1U Active Thermal Control technology (ATC) for high power payload support in 6U CubeSat form factors and above. The design utilizes a two-stage, single-phase mechanically pumped fluid loop coupled through a two-axis flexible rotary fluid hinge, to reject thermal power to a deployable tracking radiator. A COTS Ricor K508N cryocooler forms the second stage and provides cryogenic cooling to a custom Kevlar detector mount through a TMT pyrolytic graphene thermal strap. Passive vibration isolation and damping technologies prevent the transfer of jitter to the satellite systems. The ATA design utilizes state-of-the-art 3D fabrication techniques such as Ultrasonic Additive Manufacturing (UAM) to directly embed the working fluid channels into the HX, radiator, and CubeSat chassis allowing for the miniaturization and simplification of the ATA system into an integrated thermal control solution. This paper will focus on the design and ground-based characterization and qualification of the ATA system and provide performance metrics for its use as a thermal support subsystem for advanced infrared electro-optical CubeSat payloads. The ATA project is funded through a NASA Small Satellite Technology Program (SSTP) and is a partnership between the Center for Space Engineering at Utah State University and the Jet Propulsions Laboratory. The ATA active thermal control system has been raised to a TRL of 6 and hopes to provide payload support to advanced missions such as the SABER-Lite and JPL CIRAS projects.
Random Vibration, Exported Vibration and Passive Isolation Testing of the Ricor K508N Cryocooler
No abstract provided
Active Thermal Architecture for Cryogenic Optical Instrumentation (ATACOI)
The Active Thermal Architecture for Cryogenic Optical Instrumentation (ATACOI) project will demonstrate an advanced thermal control system for CubeSats and enable the use of cryogenic electro-optical instrumentation on small satellite platforms. Specifically, the project focuses on the development of a deployable solar tracking radiator, a rotationally flexible rotary union fluid joint, and a thermal/vibrational isolation system for miniature cryogenic detectors. This technology will represent a significant improvement over the current state of the art for CubeSat thermal control, which generally relies on simple passive and conductive methods.
The Scintillation Prediction Observations Research Task: An International Science Mission Using a Cubesat
No abstract available
The Scintillation Prediction Observations Research Task: A Multinational Science Mission Using a Cubesat
No abstract available
The Scintillation Prediction Observations Research Task (SPORT): an International Science Mission Using a Cubesat
The Scintillation Prediction Observations Research Task (SPORT) is a 6U CubeSat mission to address the compelling but difficult problem of understanding the preconditions leading to equatorial plasma bubbles. The scientific literature describes the preconditions in both the plasma drifts and the density profiles related to bubble formations that occur several hours later in the evening. Most of the scientific discovery has resulted from observations at a single site, within a single longitude sector, from Jicamarca, Peru. SPORT will provide a systematic study of the state of the pre-bubble conditions at all longitudes sectors to enhance understanding between geography and magnetic geometry. SPORT is an international partnership between National Aeronautics and Space Administration (NASA), the Brazilian National Institute for Space Research (INPE), and the Technical Aeronautics Institute under the Brazilian Air Force Command Department (DCTA/ITA), and encouraged by U.S. Southern Command. This talk will present an overview of the SPORT mission, observation strategy, and science objectives to improve predictions of ionospheric disturbances that affect radio propagation of telecommunication signals. The science goals will be accomplished by a unique combination of satellite observations from a nearly circular middle inclination orbit and the extensive operation of ground based observations from South America near the magnetic equator.
The Scintillation Prediction Observations Research Task (SPORT): an International Science Mission Using a CubeSat
No abstract available
The Scintillation Prediction Observations Research Task: An International Science Mission using a CubeSat
No abstract available
The Scintillation Prediction Observations Research Task: An International Science Mission using a CubeSat
No abstract available
The Scintillation Prediction Observations Research Task (SPORT) Mission Overview
No abstract available
The Scintillation Prediction Observations Research Task (SPORT) Mission
SPORT is a science mission using a 6U CubeSat and integrated ground network that will (1) advance understanding and (2) enable improved predictions of scintillation occurrence that impact GPS signals and radio communications. This is the science of Space Weather. SPORT is an international partnership with NASA, U.S. institutions, the Brazilian National Institute for Space Research (INPE), and the Technical Aeronautics Institute under the Brazilian Air Force Command Department (DCTA/ITA).
The Scintillation Prediction Observations Research Task: An International Science Mission Using a CubeSat
No abstract available
The Scintillation Prediction Observations Research Task (SPORT)
No abstract available