| Orbit Design
The Navigation and Mission Design Branch (NMDB) provides trajectory design
support for a wide
range of mission phases from feasibility studies through launch and
early orbit operations. Feasibility study support typically involves
starting with a scientist’s mission goals, producing a viable
trajectory, and providing input to subsystem designers (power, thermal,
propulsion, communications, and attitude) to ensure subsystem
feasibility for the required orbit. This support to proposal efforts,
trade studies, and requested analysis items is provided both through
the Integrated Mission Design Center (IDC) as well as independently to
assist in the definition of mission and trajectory requirements. As the
subsystems mature, further refinements to the trajectory are computed,
and interfaces are established with the launch vehicle provider, the
flight operations team, and the flight project. NMDB provides the
necessary mission analysis to meet all science and subsystem
constraints while minimizing the mission cost function (e.g. dV, time
of transfer, figure of merit). NMDB provides ground system design,
testing, and operations to ensure a robust and accurate implementation
of the control strategy . After launch, NMDB provides maneuver planning
and calibration to place the spacecraft in its mission orbit.
NMDB’s mission design experts have
been performing analysis and consultation for a wide variety of
missions including:
- Low earth
- Geosynchronous
- Geostationary
- Highly eccentric
- Libration point (Lissajous
orbit description)
- Lunar
- Gravitational assist
- Interplanetary trajectories
NMDB also has experience in many
special types of trajectory design, including:
- Formation Flying
- Constellation Design
- Frozen
Orbits
- End-of-life
spacecraft disposal
- Comet and asteroid rendezvous
- Aerobraking
NMDB interfaces with many non-NASA
entities for
mission support, including scientists and principal investigators, the
spacecraft contractor, and the launch vehicle provider. Many interfaces
are well-established and allow interactions with these entities to be
smooth and integrated into the mission design and analysis efforts.
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