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MIL-T-23426D
TENSION BAR/RELEASE ELEMENT, AIRCRAFT LAUNCHING
Organization:
NAVY - AS - Naval Air Systems Command
Year: 1986
Abstract: This specification covers requirements for the procurement of tension bars/release elements (TB/RE) of the types and part numbers shown in 1.2. Frangible elements that are used to launch nose gear launch aircraft are referred to as release elements.
The tension bar/release element (TB/RE) shall be classified by type as follows in Table I: TABLE I. Type Classification
Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be address to: NAVAL AIR ENGINEERING CENTER, SYSTEMS ENGINEERING AND STANDARDIZATION DEPARTMENT (CODE 93), Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DP Form 1426) appearing at the end of this document or by letter.
Intended Use: This specification covers TB/RE that are intended to be used in military aircraft launchings. The TB/RE are designed to break at a specific tension load to release an aircraft from a catapult.
The tension bar/release element (TB/RE) shall be classified by type as follows in Table I: TABLE I. Type Classification
TYPE TYPE OF NAEC BREAKING MATERIAL OR PART STRENGTH PROCESS NUMBER POUNDS NEWTONS ------------------------------------------------------------------------ I Hollow Bar 502822-4 28,500 ± 1500 126,774 ± 6,672 II Solid Bar 513436-1 36,200 ± 1500 161,025 ± 6,672 413745-1 38,000 ± 1500 169,032 ± 6,672 417599-1 53,000 ± 1500 235,755 ± 6,672 506409-1 63,000 ± 1890 280,737 ± 8,407 508713-1 63,000 ± 1890 280,237 ± 8,407 III Forging 517891-1 46,453 ± 1353 206,632 ± 6,018
Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be address to: NAVAL AIR ENGINEERING CENTER, SYSTEMS ENGINEERING AND STANDARDIZATION DEPARTMENT (CODE 93), Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DP Form 1426) appearing at the end of this document or by letter.
Intended Use: This specification covers TB/RE that are intended to be used in military aircraft launchings. The TB/RE are designed to break at a specific tension load to release an aircraft from a catapult.
Subject: Aircraft
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| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T18:28:21Z | |
| date available | 2017-09-04T18:28:21Z | |
| date copyright | 31712 | |
| date issued | 1986 | |
| identifier other | IQMLDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho1216AF679D40AC421854DD6EFDEC014A/handle/yse/210533 | |
| description abstract | This specification covers requirements for the procurement of tension bars/release elements (TB/RE) of the types and part numbers shown in 1.2. Frangible elements that are used to launch nose gear launch aircraft are referred to as release elements. The tension bar/release element (TB/RE) shall be classified by type as follows in Table I: TABLE I. Type Classification TYPE TYPE OF NAEC BREAKING MATERIAL OR PART STRENGTH PROCESS NUMBER POUNDS NEWTONS ------------------------------------------------------------------------ I Hollow Bar 502822-4 28,500 ± 1500 126,774 ± 6,672 II Solid Bar 513436-1 36,200 ± 1500 161,025 ± 6,672 413745-1 38,000 ± 1500 169,032 ± 6,672 417599-1 53,000 ± 1500 235,755 ± 6,672 506409-1 63,000 ± 1890 280,737 ± 8,407 508713-1 63,000 ± 1890 280,237 ± 8,407 III Forging 517891-1 46,453 ± 1353 206,632 ± 6,018 Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be address to: NAVAL AIR ENGINEERING CENTER, SYSTEMS ENGINEERING AND STANDARDIZATION DEPARTMENT (CODE 93), Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DP Form 1426) appearing at the end of this document or by letter. Intended Use: This specification covers TB/RE that are intended to be used in military aircraft launchings. The TB/RE are designed to break at a specific tension load to release an aircraft from a catapult. | |
| language | English | |
| title | MIL-T-23426D | num |
| title | TENSION BAR/RELEASE ELEMENT, AIRCRAFT LAUNCHING | en |
| type | standard | |
| page | 23 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1986 | |
| contenttype | fulltext | |
| subject keywords | Aircraft | |
| subject keywords | Launching Tension Bar/Release Element | |
| subject keywords | Launching | |
| subject keywords | Tension Bar/Release Element | |
| subject keywords | Aircraft | |
| subject keywords | Release Element/Tension Bar | |
| subject keywords | Aircraft Launching | |
| subject keywords | Tension Bar/Release Element | |
| subject keywords | Aircraft Launching. |