GB/T 29078-2012
ActiveDesign guidelines for spacecraft launch window
航天器发射窗口设计指南
Application Summary AI generated
This standard provides design guidelines for determining the launch window of spacecraft, considering orbital mechanics, mission objectives, and constraints such as ground tracking and solar illumination. It is applied in the aerospace industry for planning and executing satellite and deep-space missions, ensuring optimal launch timing for rendezvous, orbit insertion, or planetary encounters. The guidelines are used by mission designers and engineers during the pre-launch phase to calculate feasible launch periods.
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