Richard Bennett
System Engineer
Jet Propulsion Laboratory
Present Position:
Project Element Manager- Systems Engineering, Dec. 1997 to
present
Mission Systems Engineer assigned to the GENESIS Project
providing end-to-end systems engineering across all project
elements ensuring balanced, internally compatible systems.
Project Engineering - Senior, Nov. 1992 to Nov. 1997
- Team Leader of the Advanced Projects Design Team (Team-X).
Provide daily management and guidance for a seventeen member
space mission design organization. Coordinate team membership
and design processes, provide customer interface, organize
team and facility schedules, lead studies and maintain sufficient
metrics to monitor and enhance study performance.
- Project Manager assigned to the Energetic X-ray Imaging
Survey Telescope (EXIST) MIDEX Step II proposal effort.
Developed and authored investigation management plan. Designed
project implementation plan, cost and schedule. Assisted
the principal investigator in coordinating proposal technical
concepts and solutions from a group of multi-national institutions
including U.S. private universities; NASA/GSFC & MSFC; University
of Birmingham, UK; and IAS, Frascati, Italy.
- Division 34 power representative to the Advanced Projects
Design Team (Team-X). Provided power system design expertise
for integrated advanced mission studies. Also functioned
as the Electric Power Section cost estimation coordinating
engineer responsible to Division 34's Strategic Goal #2
Focus Group. Supported power systems studies and IN-STEP
RTOP management activities for the Electric Power systems
Section. Conceptualized power system designs, implementation
plans and costs for advanced studies including AIT, ACME,
MESUR network, SIR-C Free flyer and the 2nd generation µ
S/C project. Established a cost tracking and management
system for task management of the In-Space Experiment activities
including cost planning, variance analysis, earned value
and status reporting. Assisted in the coordination and evaluation
of the IN-STEP '92 AO activity. Authored section process
for design-to-cost estimation.
Previous Positions:
Hughes Aircraft Company - Space & Communications Group
1978 - 1992
- Operations Manager:
Planned, implemented and managed organization for the system
integration, test and launch of the first of a new product
line of three-axis stabilized communications satellites
(HS-601), AUSSAT B1. Developed baseline requirements and
production flow. Selected team and managed floor operations.
Defined and resolved technical issues. Maintained close
working relationship with Hughes customer, AUSSAT PTY. LTD.
and the launch vehicle services provider, China Great Wall
Industries Corporation. Managed launch site operations and
services in Xichang, China. Successfully placed first vehicle
in-orbit and on-station during August, 1992 after developing
an optimized six week ship-and-shoot campaign.
- Previous management experience: Assistant Department Manager
of 80 scientists, engineers and technicians involved in
the design and development of satellite and space shuttle
avionic control electronics. Proposed and designed fully
automated test systems. Authored test plans and procedures.
Validated systems, supervised flight hardware qualification
and acceptance programs along with general business and
financial responsibilities including proposal work, cost
account control and earned value. .
Technical Background
- Digital hardware circuit and systems production design
including. . .
- Ground system block decoders and synchronizers for
Pioneer Venus orbiter and probe system
- Memory simulators used for flight software development
on Galileo DCP, Space Shuttle Rendezvous Radar, and
IAPS experiment (Ion propulsion system)
- Telemetry & command simulator for test support of
the IAPS thrust controller
- Bit synchronizer developed to perform bit-error-rate
testing for shuttle / TDRS communication equipment
- Shuttle Rendezvous Radar backplane design for the
EA1 (a ten slice, microprocessor controlled flight avionics
unit
- Fully automatic test systems for. . .
- (1) Shuttle two-axis gimbal drive controller;
- (2) INTELSAT VI driver electronics (thruster,
valve, solenoid, squib & stepper units);
- (3) ACS electronics for several defense satellite
programs - Environmental test planning, procedures
and specifications covering Thermal (solar thermal
vacuum, temperature cycling & long duration exposure),
Vibration (sine, random & acoustic), Shock, EMI/EMC,
ESD and facilities design & setup.
Education:
California State Polytechnic University, Pomona, California
Bachelor of Science - Engineering (Electronics), December
1977
Glendale Community College, Glendale, California Associate
in Arts - June 1975 |