TECHNICAL PAPERS

DC-X Hydraulic Flight Control System

Date Published: 1995-09-01
Paper Number: 951994
DOI: 10.4271/951994

Citation:

Strode, G., "DC-X Hydraulic Flight Control System," SAE Technical Paper 951994, 1995, doi:10.4271/951994.

Author(s):


George Strode - McDonnell Douglas Aerospace

Abstract:

The first reusable rocket to land on earth has a normal hydraulic system consisting of the usual components. However, what happened when four variable displacement hydraulic pumps interact with each other was not normal; nor was it normal to experience an explosion at the beginning of Flight No. 5 that damaged the hydraulic system, but the vehicle continued to fly properly for a 78 second aborted mission.

File Size: 702K

Product Status: In Stock

See papers presented at Aerotech Conference & Exposition, September 1995, Los Angeles, CA, USA, Session: Aerotech Conference & Exposition

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