Accession Number:

AD0817468

Title:

FEASIBILITY STUDY OF FLUID FLYWHEEL TECHNIQUES TO PROVIDE NUTATION DAMPING OF LARGE SPINNING SPACE VEHICLES.

Descriptive Note:

Technical rept. Apr-Nov 66,

Corporate Author:

GENERAL ELECTRIC CO JOHNSON CITY NY LIGHT MILITARY ELECTRONICS DEPT

Personal Author(s):

Report Date:

1967-05-01

Pagination or Media Count:

106.0

Abstract:

The purpose of this study was to examine the feasibility of using fluid flywheels for nutation damping of large manned spinning space vehicles. A model space vehicle was selected, and a flywheel loop and pump analysis was conducted to define the best loop configuration and fluid-pump combination. Operational feasibility, weight and power requirements of the final system were determined by both analysis and analog simulation. It was concluded that a fluid flywheel damper system is both feasible and competitive.

Subject Categories:

  • Manned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE