Determination of Inertia Load Which The Fuel Cells In The Fuselage of The Comet Model 4 Airplane May Be Capable of Withstanding Without Rupture During Crash Conditions

doi:10.21949/1512150

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ROSA P serves as an archival repository of USDOT-published products including scientific findings, journal articles, guidelines, recommendations, or other information authored or co-authored by USDOT or funded partners. As a repository, ROSA P retains documents in their original published format to ensure public access to scientific information.

i

Determination of Inertia Load Which The Fuel Cells In The Fuselage of The Comet Model 4 Airplane May Be Capable of Withstanding Without Rupture During Crash Conditions

1957-05-01
Series: Civil Aeronautics Administration Reports

[PDF-543.74 KB]

English

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Details:

Alternative Title:

CAA Technical Development Reports
Corporate Contributors:

United States. Civil Aeronautics Authority
Subject/TRT Terms:

[+]

Airports Fuel Cells Performance Safety
Series:

Civil Aeronautics Administration Reports
DOI:

https://doi.org/10.21949/1512150
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Civil Aeronautics Authority
Abstract:

Determination of inertia load which the fuel cells in the fuselage of the comet model 4 airplane may be capable of withstanding without rupture during crash conditions.
Content Notes:

Public Domain
Format:

PDF
Collection(s):

CAA and FAA Reports
Main Document Checksum:

[+]

urn:sha-512:86f4c293ff2ae2e487c446ec9a7eb383488d2dad78dc40b66dcff78e98ac26ec6a5ecde55e72bffe17de36fb31e2eaf4690605038c2bcdcbd727688756689098
Download URL:

https://rosap.ntl.bts.gov/view/dot/81582/dot_81582_DS1.pdf
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Determination of Inertia Load Which The Fuel Cells In The Fuselage of The Comet Model 4 Airplane May Be Capable of Withstanding Without Rupture During Crash Conditions

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