NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Hatch latch mechanism for Spacelab scientific airlockThe requirements, design tradeoff, design, and performance of the Spacelab scientific airlock hatch latching mechanisms are described. At space side the hatch is closed and held against internal airlock/module pressure by 12 tangential overcenter hooks driven by a driver. At module side the hatch is held by 4 hooks driven by rollers running on a cammed driver.
Document ID
19790013190
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Terhaar, G. R. (Ver. Flugtech. Werke-Fokker G.m.b.H.)
Date Acquired
August 9, 2013
Publication Date
April 1, 1979
Publication Information
Publication: The 12th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
79N21361
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19790013181Collected WorksThe 12th Aerospace Mechanisms Symposium
No Preview Available