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Optical Extinction Measurements of Dust Density in the GMRO Regolith Test BinA regolith simulant test bin was constructed and completed in the Granular Mechanics and Regolith Operations (GMRO) Lab in 2013. This Planetary Regolith Test Bed (PRTB) is a 64 sq m x 1 m deep test bin, is housed in a climate-controlled facility, and contains 120 MT of lunar-regolith simulant, called Black Point-1 or BP-1, from Black Point, AZ. One of the current uses of the test bin is to study the effects of difficult lighting and dust conditions on Telerobotic Perception Systems to better assess and refine regolith operations for asteroid, Mars and polar lunar missions. Low illumination and low angle of incidence lighting pose significant problems to computer vision and human perception. Levitated dust on Asteroids interferes with imaging and degrades depth perception. Dust Storms on Mars pose a significant problem. Due to these factors, the likely performance of telerobotics is poorly understood for future missions. Current space telerobotic systems are only operated in bright lighting and dust-free conditions. This technology development testing will identify: (1) the impact of degraded lighting and environmental dust on computer vision and operator perception, (2) potential methods and procedures for mitigating these impacts, (3) requirements for telerobotic perception systems for asteroid capture, Mars dust storms and lunar regolith ISRU missions. In order to solve some of the Telerobotic Perception system problems, a plume erosion sensor (PES) was developed in the Lunar Regolith Simulant Bin (LRSB), containing 2 MT of JSC-1a lunar simulant. PES is simply a laser and digital camera with a white target. Two modes of operation have been investigated: (1) single laser spot - the brightness of the spot is dependent on the optical extinction due to dust and is thus an indirect measure of particle number density, and (2) side-scatter - the camera images the laser from the side, showing beam entrance into the dust cloud and the boundary between dust and void. Both methods must assume a mean particle size in order to extract a number density. The optical extinction measurement yields the product of the 2nd moment of the particle size distribution and the extinction efficiency Qe. For particle sizes in the range of interest (greater than 1 micrometer), Qe approximately equal to 2. Scaling up of the PES single laser and camera system is underway in the PRTB, where an array of lasers penetrate a con-trolled dust cloud, illuminating multiple targets. Using high speed HD GoPro video cameras, the evolution of the dust cloud and particle size density can be studied in detail.
Document ID
20160005055
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Lane, J.
(Enterprise Advisory Services, Inc. (EASI) FL, United States)
Mantovani, J.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Mueller, R.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Nugent, M.
(Sierra Lobo, Inc. Kennedy Space Center, FL, United States)
Nick, A.
(Sierra Lobo, Inc. Kennedy Space Center, FL, United States)
Schuler, J.
(Enterprise Advisory Services, Inc. (EASI) FL, United States)
Townsend, I.
(Craig Technologies Cape Canaveral, FL, United States)
Date Acquired
April 14, 2016
Publication Date
April 11, 2016
Subject Category
Optics
Report/Patent Number
KSC-E-DAA-TN27566
Report Number: KSC-E-DAA-TN27566
Meeting Information
Meeting: ASCE International Conference on Engineering, Science, Construction and Operations in Challenging Environments (Earth and Space 2016)
Location: Orlando, FL
Country: United States
Start Date: April 11, 2016
End Date: April 15, 2016
Sponsors: American Society of Civil Engineers
Funding Number(s)
CONTRACT_GRANT: NNK11EA08C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
lunar simulant
optical extinction
dust
regolith
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