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bd
Systems has been a major player in space and launch systems
development throughout the history of the company. Our staff
has provided a broad range of direct engineering and
technical support to Rocketplane, the Orbital Space Plane
program, Reusable Launch Vehicle program, Evolved Expendable
Launch Vehicle program, and the Titan and Delta II programs.
We have also provided direct support to NASA Marshall Space
Flight Center on numerous space programs over the past 15
years.
Crew
Exploration Vehicle – CEV (Northrop Grumman/Boeing)
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Systems is providing broad systems engineering support to
Northrop Grumman and Boeing in support of NASA’s Crew
Exploration Vehicle (CEV). We have staff integrated with the
NG/Boeing team supporting CEV systems requirements
definition, internal and external interfaces, EVA operations
including architecture and design, and mission and launch
operations.
Rocketplane
XP (Rocketplane Limited Inc.)
We
are a significant contractor on the development of the
Rocketplane XP suborbital transportation system, developing
and delivering the guidance, navigation and control (GN&C)
subsystem to the project and providing major analysis and
design engineering for the airframe structure. We are lead
developer of the vehicle control system and are providing
comprehensive vehicle analysis, encompassing structures, GN&C,
thermal. Developing ground-up GN&C architecture and
preliminary flight code, including flight modes, and closed
loop ascent guidance.
Orbital
Space Plane – OSP (Boeing)
Broad
in scope, bd Systems support for Boeing’s OSP program
included systems definition, modeling & simulation,
systems engineering, and discrete design & integration
tasks. We assisted Boeing in a number of systems engineering
functions during the transition from the Re-useable Launch
Vehicle program to the initial OSP concept including
requirements definition, validation/verification planning,
analyses and trades leading to design solutions. We
performed functional analyses (FFBDs and IDEFOs) and
timeline analyses for the OSP and provided structure and
technical support for populating the DOORS requirements tool
used by Boeing. Boeing also assigned bd Systems to develop
key OSP documentation including the system specifications,
element specs, and ICDs. Our engineering staff also
performed aerodynamic analyses and testing. We also used our
tools, facilities, and resources to perform a number of
analytical and modeling and simulation tasks for Boeing. In
addition, we assisted in developing the spacecraft segment
specification, resource module element specification, and
selected ICDs.
Space
Transportation System (United Space Alliance)
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Systems performs structural and modal analysis, modal
testing, mechanical simulations of highly non-linear
transient systems, strength analysis of metallic and
composite structures, fatigue and crack growth analysis,
vibroacoustic analysis and neural network applications
development. bd performs this type of work as part of our
support to the United Space Alliance for each shuttle
flight.
Reusable
Launch Vehicle - RLV (Boeing)
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Systems also provided subcontractor support to Boeing for
the RLV program. This support was broad in scope and
included architectural definition studies, modeling &
simulation, systems engineering, and a variety of design
& integration tasks. bd engineers assisted Boeing to
develop alternate RLV architecture concepts, support
parametric analyses, perform architecture trades, and
develop the RLV functional architecture. We also assisted in
a number of systems engineering functions with primary focus
on requirements definition. We were also tasked to develop
key RLV documentation including an RLV operational
requirements document and ICDs. We prepared evolution
studies including the RLV
Space Futures Report and provided support in specialty
areas of reliability engineering and configuration
management. In addition, we performed a number of analytical
and modeling & simulation tasks including
Booster/Orbiter/Payload separation, docking, berthing, and
landing. bd engineers also supported RLV wind tunnel tests
including performance of moment and aero-thermal analyses of
various configurations.
Evolved
Expendable Launch Vehicle – EELV (USAF Space & Missile
Systems Center)
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Systems provides a variety of program management and
engineering support to the EELV program managed at SMC.
Technical support included front-end development of system
requirements, cost-trade analyses, reliability planning
& analysis, configuration management and information
services, and also included support to EELV test and
evaluation support to the Air Force Operational Test and
Evaluation Center (AFOTEC) at Kirtland AFB, New Mexico. A
significant amount of on-going support is acquisition and
program management in nature and includes preparation of
contract technical data packages, development of request for
proposal instructions, source selection guidelines,
criteria, and support of acquisition strategy development.
Titan
IV Launch System (USAF SMC)
Our
staff has significant support experience in the
development and operational launch of Titan IV. We have
participated in design and performance verification testing
and analyses on Titan IV components as well as material
property characterization programs, and were major
contributors in developing and implementing motor life tests
and analyses to validate service life requirements. We also
developed integrated processes to eliminate possible failure
scenarios and led “proof of failure” test efforts. A
member of our staff led an investigation team to identify
all potential rocket motor failure modes following a Titan
IV launch failure. Our team has also provided specialty
support including quality engineering and
configuration management.
Delta
Launch System (USAF SMC & McDonnell Douglas)
Members
of our engineering team have experience in development and
operational launch of Delta II launch system. bd staff
members participated in the evolution of the Delta to the
Delta II following the Space Shuttle Challenger accident,
and are experienced in the integration of the various
payloads on Delta II including GPS and a variety of NASA
payloads including ROSAT and others. Our team also
participated in the first independent readiness review (IRR)
performed on the Delta II.
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