Distinguished Guest Lecturer: Brian M. Kent
TITLE: Characterization of Space Shuttle Ascent Debris
Based on Radar Scattering and Ballistic Properties –
Evolution of the NASA
Debris Radar (NDR) System
Date: Tuesday, September 23, 2014 Time: 3:00 PM
Location: MIT Lincoln Laboratory (Auditorium) Refreshments served at 2:30pm
Abstract: This presentation (with optional break) introduces the NASA Debris Radar (NDR) system developed to characterize debris liberated by the space shuttle (and any follow-on rocket system) during its ascent into space. Radar technology is well suited for characterizing shuttle ascent debris, and is especially valuable during night launches when optical sensors are severely degraded. The shuttle debris mission presents challenging radar requirements in terms of target detection and tracking, minimum detectable radar cross-section (RCS), calibration accuracy, power profile management, and operational readiness. After setting the stage with background of the Columbia accident, I initially describe the NDR system consists of stationary C-band radar located at Kennedy Space Center (KSC) and two X-band radars deployed to sea during shuttle missions. To better understand the signature of the shuttle stack, Xpatch calculations were generated at C and X band to predict the radar signature as a function of launch time. These calculations agreed very well with measured data later collected. Various sizes, shapes, and types of shuttle debris materials were characterized using static and dynamic radar measurements and ballistic coefficient calculations. After an (Optional) break, my second Part discusses the NASA Debris Radar (NDR) successes, which led to a new challenge of processing and analyzing the large amount of radar data collected by the NDR systems and extracting information useful to the NASA debris community. Analysis tools and software codes were developed to visualize the shuttle metric data in real-time, visualize metric and signature data during post-mission analysis, automatically detect and characterize debris tracks in signature data, determine ballistic numbers for detected debris objects, and assess material type, size, release location and threat to the orbiter based on radar scattering and ballistic properties of the debris. Future applications for space situational awareness and space-lift applications will also be discussed.
For more information, contact:
Raoul O. Ouedraogo, raoul.o...@ll.mit.edu
Wajih Elsallal, wels...@mitre.org , or
Jonathan Doane, jon....@ll.mit.edu
Please
contact Jonathan Doane to RSVP or if you are interested in attending remotely
via WebEx before 9-22-2014.
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Dr. Brian M. Kent is a Consultant in Aerospace, Science, and Technology, and an adjunct professor of Electrical Engineering with Michigan State University's Department of Electrical Engineering. He recently completed 37 years of Service to the United States Air Force having most recently served as the Chief Technology Officer of Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio. As CTO, he was AFRL’s principal scientific and technical expert for a 6,500 person organization while overseeing a $2.2B+ research portfolio. He is an internationally recognized scientific expert, and provided technical advice to AFRL management and the professional staff. He has significant experience in engineering education, radar, radar signature, and other radio frequency technologies. He is currently a consultant supporting both academic, and industrial partners related to the aerospace industry.
During his previous tenure as AFRL’s
Sensor’s Directorate Chief Scientist, he served as the directorate's
principal scientific and technical adviser and primary authority for the
technical content of the science and technology portfolio. He identified research
gaps and analyzes advancements in a broad variety of scientific fields,
providing advice on their impact on laboratory programs and objectives. He
served as an internationally recognized scientific expert, and provided
authoritarian counsel and advice to AFRL management and the professional
staff as well as to other government organizations. He collaborated on
numerous interdisciplinary research problems that encompass multiple AFRL
directorates, customers from other DOD components, as well as the manned
space program managed by NASA.
Dr. Kent joined the Air Force
Avionics Laboratory in 1976 as cooperative engineering student through
Michigan State University. He received a National Science Foundation
Fellowship in 1979, working at both the Air Force Wright Aeronautical
Laboratories and the Ohio State University Electroscience Laboratory until
the completion of his doctorate. During his tenure with AFRL and its
predecessor organizations, Dr. Kent held a variety of positions, making pioneering
and lasting contributions to the areas of signature measurement technology,
and successfully established international standards for performing radar
signature testing before retiring from the USAF after 37 years of service.
Dr. Kent has authored and
co-authored more than 90 archival articles and technical reports and has
written key sections of classified textbooks and design manuals. He has
delivered more than 200 lectures, and developed a special DOD Low Observables
Short Course that has been taught to more than 3,000 scientists and engineers
since its inception in 1989. Dr. Kent has provided technical advice and
counsel to a wide range of federal agencies, including the Department of
Transportation, the Department of Justice and NASA's Space Shuttle Program.
He is also an international technical adviser for the DOD and has provided
basic research guidance to leading academic institutions. 2014 Claude Erickson Distinguished Engineering Alumni Award, Michigan State University 2009 Meritorious Presidential
Rank Award Fellow,
Institute of Electrical and Electronic Engineers |