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| 01960nam 2200313za 4500 |
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001 | 9.821199 |
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003 | CaOODSP |
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005 | 20240219183437 |
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007 | cr ||||||||||| |
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008 | 160718s2011 onc|||||o f000 0 eng d |
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040 | |aCaOODSP|beng |
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041 | |aeng|bfre |
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043 | |an-cn--- |
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086 | 1 |aD68-5/116-2011E-PDF |
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100 | 1 |aMartell, Bill. |
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245 | 10|aLP/SV bladder buoyancy test comparison |h[electronic resource] / |cby Bill Martell and Ryan Wolter. |
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260 | |a[Ottawa] : |bDefence Research and Development Canada, |cc2011. |
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300 | |aiv, 14 p. : |bfigures. |
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490 | 1 |aTechnical Note ; |v2011-116 |
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500 | |a"July 2011." |
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504 | |aIncludes bibliographical references. |
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520 | |aBackground: The buoyancy of CF jet aircrew LP/SV is unknown and may not provide the minimum 35 lbs that is required. The buoyant force of the British MK 30 LCX is also unknown; however, this flotation device utilizes a large bladder and may replace the LP/SV. Aim: The aim of this experiment was to calculate and compare the buoyant force of the CF LP/SV and the British MK 30 LCX. Methods: Bladders were inflated using either a 35g or a 45g CO2 canister. A Chatillon spring scale was used to measure the buoyant force following submersion. Results: The LP/SV and MK 30 LCX attained buoyant forces of 41 and 42 lbs respectively following inflation using a 35g CO2 canister, and 45 and 53 lbs respectively following inflation using a 45g CO2 canister. Conclusion: In all trials, both flotation devices produced buoyant forces greater that 35 lbs. The British MK 30 LCX produced larger buoyancy forces. |
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692 | 07|2gccst|aTechnical reports |
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693 | 4|aLife preserver |
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693 | 4|aSafety vest |
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700 | 1 |aWolter, Ryan. |
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710 | 2 |aDefence R&D Canada. |
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830 | #0|aTechnical note (Defence R&D Canada)|v2011-116|w(CaOODSP)9.820563 |
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856 | 40|qPDF|s868 KB|uhttps://publications.gc.ca/collections/collection_2016/rddc-drdc/D68-5-116-2011-eng.pdf |
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