EVALUATION OF ERECTION MECHANISM SPEED REDUCER,

Abstract

The object of this test was to determine the effect of temperature upon the performance of the missile erection speed reducer and to structurally proof-load the reducer at high, low and ambient temperatures. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 25, 1959
Accession Number
AD0833374

Entities

People

  • Stanley B. Hendrickson

Organizations

  • General Dynamics

Tags

Fields of Study

  • Agricultural and Food sciences

Readers

  • Electrical Engineering
  • Fluid Dynamics.
  • Software Engineering