NASA Office of Logic Design

NASA Office of Logic Design

A scientific study of the problems of digital engineering for space flight systems,
with a view to their practical solution.


Richard Katz, NASA Office of Logic Design

Richard B. Katz

EDUCATION:

B.S.E.E. 1982  State University of New York at Stony Brook
  • Majors: Computer Science; Applied Mathematics and Statistics
  • Minor:   Mathematics
M.S.E.E. 1983 State University of New York at Stony Brook, EE: Computer Engineering and Digital Systems.

RESEARCH INTERESTS:

Design of high-reliability circuits. Use of programmable elements and devices in space-flight applications. High-performance microelectronics and signal processing applications.

 

EXPERIENCE:

1991-present NASA Goddard Space Flight Center.  Head, Office of Logic Design.
1989-91 ST Systems, Corp. (NASA/GSFC Contractor)
1988-89 Hewlett-Packard Corporation
1984-88 Jet Propulsion Laboratory/California Institute of Technology
1982-83 Research and Teaching Assistant, State University of New York at Stony Brook
1981, 83 Summer Intern, McDonnell-Douglas Automation Co. Flight test
1982 Summer Intern, General Instrument Corp. Minicomputer and radar simulator.

      PUBLICATIONS and PRESENTATIONS (many of the papers followed conference presentations):

Short Courses/Seminars

Conferences, Invited Talks, Papers, Columns, Reports, and Other Publications

The following NASA Tech Briefs:

http://www.klabs.org A www site dedicated to the research, development, and use of programmable logic and elements for space-flight applications.

HONORS AND PROFESSIONAL SOCIETIES:

KEY SPACE-FLIGHT PROJECTS:

Lunar Reconnaissance Orbiter: Lunar Orbiter Laser Altimeter
Solar Dynamics Observatory (SDO), Ka-band Transmitter
NESC Independent Testing of Field Programmable Gate Arrays (FPGAs)
Industry Tiger Team
, FPGA Reliability
Cockpit Avionics Upgrade Tiger Team
, FPGA Applications
Small Diameter Bomb
Independent Assessment Team
FPGA Reliability
Independent Assessment Team (MER, MRO).
DAWN Laser Altimer: Range Measurement Unit design
Astro-E2:
Independent Review and Analysis
AURA:
Residual Risks Caucus
GALEX:
Independent Assessment Team
HIRDLS Independent Assessment Team
GLAST Independent Assessment Team
ST-5 Independent Assessment Team
Second Generation Reusable Launch Vehicle
: Independent Technology Risk Assessment Team.
GRACE:
Independent Assessment Team
SORCE:
Independent Assessment Team
Messenger MLA:
Range Measurement Unit design
Mars Odyssey:
Independent Assessment Team
HETE-2:
Independent Assessment Team
WIRE:
Lead investigator for failure mechanism.
Galileo: Design/test engineer for attitude control electronics.
Magellan: Design/test engineer for attitude control electronics.
Magellan: Lead engineer for synthetic aperture radar digital units.
Intelsat VII: Consultant for digital electronics.
ISTP: Instrumentation, particle detectors, facility electronics, and high-voltage power supplies for WIND and Polar instruments.
Cassini: Algorithms and circuits for several science instruments.
SMEX/FAST: Uplink, Downlink, and ACS card designs.
IR Polaris: Detector array timing & control, data acquisition, for infrared camera.
MOLA-II: Mars Global Surveyor instrument. Laser timing, clocking, and control; improved oven 100 MHz oscillator.
IRAC/SIRTF:Digital signal processor design.
XRS: S/C Communications. MIL-STD-1553B and RS-422 interface design.
EO-1: High-speed back plane chipset design. 32-bit bus and ‘standard’ functions.
Hydrostar: High-speed digital signal processor design for cross-correlators and FIR filters.
Radiation Test and analysis of advanced components: Programmables, ASICs, high-speed memories, high-speed ADC’s, high-precision DACs, programmable substrates, antifuses.
MPTB: Flight test of advanced technology FPGAs.
STRV-1d: Flight test of advanced technology programmables (memories, PAL, FPGA, programmable substrate, etc.).
DDF Director Discretionary Fund: Principal Investigator for radiation shielding, KGD, and antifuse reliability research and development projects. Recently awarded study for FPGA-based System on Chip for Space Flight Applications.


Home - NASA Office of Logic Design
Last Revised: November 08, 2007
Digital Engineering Institute
Web Grunt: Richard Katz
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