Sentence examples for specific spacecraft from inspiring English sources

SHIELDS also includes a post-processing tool designed to calculate the surface charging for specific spacecraft geometry using the Curvilinear Particle-In-Cell (CPIC) code that can be used for reanalysis of satellite failures or for satellite design.

For example, orbital debris models like ORDEM 3.0 could be used to propagate "witness plates" in specific, high-value orbits that are standard sizes or represent specific spacecraft to determine the spatial density or flux of debris (Stansbery and Matney 2014).

When Lovell was rotated to the prime crew, no one with experience on CSM-103 (the specific spacecraft used for the mission) was available, so Aldrin was moved to CMP and Fred Haise brought in as backup LMP.

The specific spacecraft systems would also be evaluated and tested, and the worldwide tracking and communications network would be tested to see how well it would stand up in an extended mission.

To facilitate the joint analysis of GNSS observations and satellite laser ranging measurements, laser retroreflector array coordinates consistent with the IGS-specific spacecraft frame conventions are provided in addition to representative antenna offset values for all GNSS constellations.

This article discusses the attitude modes employed by present Global (and Regional) Navigation Satellite Systems (GNSSs) and the models used to describe them along with definitions of the constellation-specific spacecraft body frames.

For more details on the conventions for constellation-specific spacecraft body frames can be found in Montenbruck (2015).

Moreover it was established that specific payload and spacecraft technology development would be required to realise such a programme.

Finally, although border line with the above purpose of this paper, we also discuss multi-spacecraft specific issues and issues related to the on-board execution of the plan update system (PUS).

This means the Restore-L design has met initial mission requirements, and will now move on to a more detailed design phase to flesh out the specifics of the spacecraft SSR will construct with a launch window target of 2020.

Based on the proposed dynamical model, the energy-optimal open-loop trajectories of control inputs, namely, the required specific charges of Lorentz spacecraft, for Lorentz-propelled spacecraft formation establishment or reconfiguration problems with both fixed and free final conditions constraints are derived via Gauss pseudospectral method.