Apollo Guide

 
   

Apollo 11 Landing Site

Apollo 15 SWS

Solar Wind Spectrometer

Measures the solar wind at the lunar surface, the general properties of the solar wind, and its interaction with the Moon.

 

 

Normal Operations

 The solar wind is composed of matter ejected continuously from the Sun that spreads throughout the Solar System. The energy, density, direction of travel, and its variations were measured by the SWS. Seven sensors were located under dust shields, allowing a study of the solar wind at the lunar surface, the general properties of the solar wind and its interaction with the Moon. The solar wind stretches the Earth’s magnetic field out behind the Earth, beyond the Moon’s orbit, so the SWS also studied the Earth’s magnetic tail when the Moon passed through it. The SWS found the solar wind behaved the same as in free space outside the Earth’s magnetic tail and is slightly disturbed in the geomagnetic transition region.

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Non - Normal

 An unexpected problem with the first ALSEP on Apollo 12 involved the cables that connected the various experiment modules to the Central Station. Although the cables were fairly stiff, on Earth they tended to lie flat to the ground, held down by their own weight. However, on the Moon, the cables hardly seemed to notice the one sixth gravity and retained loops and bends they had acquired during storage inside the LM - loops that stood up from the ground rather like sections of a frozen garden hose. There were no disastrous tripping episodes during Apollo 12 such as occurred on Apollo 16, but the need to dodge cable loops slowed the astronaut's work.

 

 

 

 

 

 

Schematics

 

SWS Diagram

   

 

  Lunar Module Vehicle Familiarization Manual : LM 10 Through LM14 by [Edward Rafacz]

 

Lunar Module

 Kindle Edition

This Lunar Module Vehicle Familiarization Manual has been prepared as an aid for orientation and indoctrination purposes only. It describes the LM mission, structure, subsystems, and ground support equipment, including modifications being incorporated into LM' s 10 through 14 to support increased lunar mission requirements.

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