CA521575A - Metal carbonise et methode pour sa fabrication - Google Patents

Metal carbonise et methode pour sa fabrication

Info

Publication number
CA521575A
CA521575A CA521575A CA521575DA CA521575A CA 521575 A CA521575 A CA 521575A CA 521575 A CA521575 A CA 521575A CA 521575D A CA521575D A CA 521575DA CA 521575 A CA521575 A CA 521575A
Authority
CA
Canada
Prior art keywords
making
carbonized metal
carbonized
metal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA521575A
Other languages
English (en)
Inventor
B. Diffenderfer John
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RCA Corp
Original Assignee
Radio Corporation of America
Publication date
Application granted granted Critical
Publication of CA521575A publication Critical patent/CA521575A/fr
Expired legal-status Critical Current

Links

CA521575A Metal carbonise et methode pour sa fabrication Expired CA521575A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA521575T

Publications (1)

Publication Number Publication Date
CA521575A true CA521575A (fr) 1956-02-07

Family

ID=35674797

Family Applications (1)

Application Number Title Priority Date Filing Date
CA521575A Expired CA521575A (fr) Metal carbonise et methode pour sa fabrication

Country Status (1)

Country Link
CA (1) CA521575A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5855828A (en) * 1994-06-06 1999-01-05 Ultramet Method of forming a composite structure such as a rocket combustion chamber

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5855828A (en) * 1994-06-06 1999-01-05 Ultramet Method of forming a composite structure such as a rocket combustion chamber

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