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Slide Release DeviceA prototype release mechanism is discussed which is interchangeable with the existing orbiter/external tank separation bolt and offers reduced weight, shock, and cost. The components are reuseable. The unit takes maximum advantage of the shank diameter and installs in the monoball just as does the shear bolt, by threading in the completely assembled condition. Actuation is different, in that instead of axially breaking the shank by very high pressure (on the order of 60,000 psi) using a very large force (over 235, 000 pounds), this mechanism releases the shank by cross-axis movement against a lubricated surface. Once free, the shank is driven out of the monoball by an axially precompressed spring. Final weight can be as low as 30 pounds, and the cartridge contains less than one gram of powder. The components show no significant wear after eleven actuations under load.
Document ID
19810021631
Acquisition Source
Johnson Space Center
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
March 31, 1981
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-161048
Ref: 3F-1024-IO-10
REPT-8745
Report Number: NASA-CR-161048
Report Number: Ref: 3F-1024-IO-10
Report Number: REPT-8745
Accession Number
81N30170
Funding Number(s)
CONTRACT_GRANT: NAS9-16169
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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