NTRS - NASA Technical Reports Server

Back to Results
Fifth Aerospace Mechanisms SymposiumConference of structural design principles and mechanical engineering methods for aerospace mechanisms used in orbital and space flights
Document ID
Document Type
Special Publication (SP)
Date Acquired
September 2, 2013
Publication Date
January 1, 1971
Subject Category
Report/Patent Number
Distribution Limits
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19720005742.pdf STI

Related Records

IDRelationTitle19720005743Analytic SubsidiaryThe Apollo docking system19720005744Analytic SubsidiaryDynamic behavior of the mercury damper19720005745Analytic SubsidiaryAerospace vehicle separation mechanisms selection, design, and use considerations19720005746Analytic SubsidiaryRotary relay for space power transfer19720005747Analytic SubsidiaryResponse characteristics of a thermal-heliotrope solar-array orientation device19720005748Analytic SubsidiaryDocking-mechanism attenuator with electromechanical damper19720005749Analytic SubsidiaryDamper design from a structural engineer's point of view19720005750Analytic SubsidiaryThermomechanical piston pump development19720005751Analytic SubsidiaryIntroduction to passive nutation dampers19720005752Analytic SubsidiaryNutation dampers for single-spin satellites19720005753Analytic SubsidiaryNutation-damper design for dual-spin spacecraft19720005754Analytic SubsidiaryLow nutation-rate dampers19720005755Analytic SubsidiaryNutation dampers for manned spacecraft19720005756Analytic SubsidiaryA scanning mirror system for the Apollo telescope mount ultraviolet spectroheliometer19720005757Analytic SubsidiaryA release mechanism with mechanical redundancy19720005758Analytic SubsidiaryAccelerated vacuum testing of long life ball bearings and sliprings19720005759Analytic SubsidiaryA motor canister designed for prolonged operation in space19720005760Analytic SubsidiaryEffects of energy dissipation in the bearing assemblies of dual-spin spacecraft19720005761Analytic SubsidiaryMetal-silicate friction in ultrahigh vacuum19720005762Analytic SubsidiaryMeeting the challenge of a 50000-hour-life-time requirement19720005763Analytic SubsidiaryA lightweight bimetallic actuator for spacecraft thermal control19720005764Analytic SubsidiaryThe Apollo 11 laser ranging retro-reflector array19720005765Analytic SubsidiaryDevelopment of payload subsystem-primate mission-Biosatellite program19720005766Analytic SubsidiaryThe Mariner Mars 1971 gimbal actuator