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Large spacecraft antennas - New geometric configuration design concepts

Oliver, R. E · 1971 · 5 pictures

A 1971 NASA technical report by R. E. Oliver proposing geometric configurations for large spacecraft antennas, written for aerospace engineers designing reflector systems. The plates are line-drawn ray diagrams of parabolic and hyperbolic reflectors, dashed axes, labeled foci and angles, and arrowed ray paths — usable as schematic linework, arrow vocabulary, and technical annotation layouts.

Interplanetary spacecraft · Liquid rocket propellants · Solid propellant rocket engines · Space simulators · Technologies · Low thrust propulsion · Mission planning · Physiological effects · Spacecraft components · Telemetry · Combustion control · Computer aided design · Interplanetary flight

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