Selection of a Least "Cost" Hydraulic System for Launch Vehicle Engine Position Control Denver Div., Martin Company

Format:

Conference/Event

Author/Creator:

Moody, D. R., author.

Conference Name:

Aerospace Fluid Power Systems and Equipment Conference (1965-05-18 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1965

Summary:

The general aspects of selecting an optimum or least cost hydraulic thrust vector control system is covered. Cost includes: l) development cost, 2) unit cost, 3) the cost of weight, 4) the cost of failures, 5) the cost of low system response, 6) the cost of a short system life or operating time and 7) the cost of a long development time. This paper describes the development of a computer program for system cost investigations. The need for such investigations is discussed and results for a few specific systems presented

Notes:

Vendor supplied data

Publisher Number:

650319

Access Restriction:

Restricted for use by site license