Theory of prediction of solar eclipse as observed from a sounding rocket using rocket trajectory and eclipse ephemerisThe present paper deals with the problem of determining various solar eclipse variables as observed from a sounding rocket for various rocket trajectories. By applying the methods described to a set of trajectories, a set of boundary conditions, launch azimuth, quadrant elevation, and launch time may be selected to optimize any aspect of eclipse observation within the constraints imposed by rocket performance.
Document ID
19790041760
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mcgarvey, J. F. (NASA Goddard Space Flight Center Sounding Rocket Div., Greenbelt, Md., United States)