Systems
Engineering & Integration
ZIN Technologies has experience developing complex aerospace
systems for a wide range of carrier vehicles and has proven
that development cost can only be effectively controlled by
rigorous systems engineering and integration expertise. All
requirements (external and internal) are carefully analyzed
to determine the impact on system complexity (performance,
cost, and schedule) to ensure that they provide beneficial
constraints on the system design. Once accepted, these requirements
are carefully tracked throughout the design process and verified.
Integration activities include requirement negotiation with
carriers and safety. In addition, crew training, carrier data
products, and launch-site support agreements are created.
Ground System Design & Operations
ZIN Technologies has extensive experience in the development,
operation and maintenance of telescience support centers for
operation of instruments on the Space Shuttle and the International
Space Station with over ten years experience with the Huntsville
Operations Support Center (HOSC) at the NASA Marshall Space
Flight Center, and the Telescience Support Center (TSC) at
the NASA Glenn Research Center. During that period, the TSC
has developed from a limited control center for display of
data, to a fully functional command and control center supporting
complete control of flight instruments. The TSC includes an
array of ground support equipment, including commanding; telemetry
receipt, distribution and archiving; multiple audio channels;
multiple video channels; and secure and public web and file
servers.
In development
support of the TSC, ZIN Technologies has contributed to the
development of requirements, system architecture, specifications,
and procurement of hardware and software, implementation of
the systems, and formal verification of operability. ZIN Technologies
has specific strengths in data acquisition, distribution,
and storage. ZIN Technologies has worked closely with various
NASA (MSFC, GFSC and GRC) organizations in developing and
testing the technologies, interfaces and protocols required
to support the needs of payload developers that use these
facilities. In particular, the recent development of the capabilities
to support operations on the ISS have required the development
and testing of many new interfaces, with iterative development
by all participating organizations.
The
data systems have been developed to address the competing
constraints of minimizing development and operating costs;
maximizing availability, operability and restorability; and
addressing the concerns of security and the proprietary nature
of some data.
Verification
A verification
program is conducted to ensure that all verification requirements
(program/science, safety, assurance, interface and operational)
for the space flight payload are satisfied. Upon inception,
verification requirements are provided by the facility, vehicle
or governing NASA center, but may also be imposed by the payload
itself. Science requirements from investigators and scientists
typically evolve into requirements and "desirements," which
must also be verified. Payload development teams begin to
develop hardware that can meet those needs, as well as stay
within good engineering practices established through years
of space flight experience. Knowing how the payload
should be designed and tested directs the team to define their
own set of requirements that may not be contractually required,
but will provide confidence for the design, assembly and testing
of the payload.
Safety
and assurance requirements are of the highest priority in
verification identification, tracking and completion. These
requirements may not only affect the safety of the astronauts
and crew, but the ground team and project assigned to build
and test the payload as well. These requirements are developed
from the governing vehicle documentation, which are updated
on a frequent basis.
Verification
tracking activities are not completed until stowage on-board
the launch vehicle, and sometimes later. Tracking the many
elements of the payload, by location, purpose, and physical
status is an important part of the verification process. This
continues through launch and on-orbit operations, and will
identify if re-verification on-orbit is necessary.
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