MiniCarb: a passive, occultation-viewing, 6U CubeSat for observations of CO2, CH4, and H2O

被引:0
作者
Wilson, Emily L. [1 ]
Riot, Vincent J. [2 ]
DiGregorio, A. J. [3 ]
Ramu, Guru [4 ]
Cleveland, Paul [5 ]
Simms, Lance M. [2 ]
Carter, Darrell [2 ]
Bruner, Bill [2 ]
Young, Jennifer [6 ]
Villanueva, Geronimo [1 ]
机构
[1] NASA Goddard Space Flight Ctr, Greenbelt, MD 20771 USA
[2] Lawrence Livermore Natl Lab, 7000 East Ave, Livermore, CA USA
[3] Amer Univ, 4400 Massachusetts Ave NW, Washington, DC USA
[4] Mach 33 Engn, 14703 Exbury Lane, Laurel, MD USA
[5] Energy Solut Int, 19630 Hoover Farm Dr, Laytonville, MD USA
[6] Genesis Engn, 4501 Boston Way, Lanham, MD USA
关键词
CubeSat; laser heterodyne radiometer; greenhouse gases; methane; carbon dioxide; water vapor; LASER HETERODYNE RADIOMETER; COLUMN;
D O I
10.1088/1361-6501/ac3679
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
We present the final design, environmental testing, and launch history of MiniCarb, a 6U CubeSat developed through a partnership between NASA Goddard Space Flight Center and Lawrence Livermore National Laboratory. MiniCarb's science payload, developed at Goddard, was an occultation-viewing, passive laser heterodyne radiometer for observing methane, carbon dioxide, and water vapor in Earth's atmosphere at & SIM;1.6 & mu;m s(-1). MiniCarb's satellite, developed at Livermore, implemented their CubeSat Next Generation Bus plug-and-play architecture to produce a modular platform that could be tailored to a range of science payloads. Following the launch on 5 December 2019, MiniCarb traveled to the International Space Station and was set into orbit on 1 February 2020 via Northrop Grumman's Cygnus capsule which deployed MiniCarb with tipoff rotation of about 20 & DEG; s(-1) (significantly higher than the typical rate of 3 & DEG; s(-1) from prior CubeSats), from which the attitude control system was unable to recover resulting in a loss of power. In spite of this early failure, MiniCarb had many successes including rigorous environmental testing, successful deployment of its solar panels, and a successful test of the radio and communication through the Iridium network. This prior work and enticing cost (approximately $2 M for the satellite and $250 K for the payload) makes MiniCarb an ideal candidate for a low-cost and rapid rebuild as a single orbiter or constellation to globally observe key greenhouse gases.
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页数:10
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