00000nam 2200000zi 4500 9.934142 CaOODSP 20240219160719 m o d f cr |n||||||||| 240219e197212uuqucad obt f000 0 eng d CaOODSP eng rda CaOODSP eng fre n-cn-qu DR52-7/3-1971E-PDF Leech, C., author. 2.75-inch rocket vehicle assessment : an evaluation of 2.75-inch folding fin aircraft rocket (FFAR) delivery errors (u) / by C. Leech. Québec, Canada : Centre de recherches pour la défense [Valcartier] = Defence Research Establishment Valcartier, December/décembre 1972 1 online resource (ii, 47 pages) : illustrations, charts text txt rdacontent computer c rdamedia online resource cr rdacarrier DREV technical note ; no. 2048/72 Cover title. "PROJ. 10-29-05"--cover page. Digitized edition from print [produced by Defence Research and Development Canada]. Includes bibliographical references (page 13). "The selection of rockets for use in aircraft employed in the ground strike role, is based in part upon the delivery accuracy of the aircraft-rocket system. The contributing error components, defined as aiming error, ballistic error and ballistic dispersion are assessed. It is found that the ballistic dispersion is significantly smaller than the ballistic and aiming errors. The contribution of bias, whether it comes from the pilot or the system was considered, especially the effect of bias and dispersion on total hit probability. The analysis was applied to the MK-4 and the MK-40 2.75-inch folding fin aircraft rockets when launched from CF-104 aircraft."--abstract (page i). Includes abstract in French. Air-to-surface missiles Testing. Ballistics. Missiles air-sol Essais. Balistique. Technical reports lcgft Rapports techniques rvmgf Defence Research Establishment Valcartier, issuing body. DREV technical note ; no. 2048/72. (CaOODSP)9.934072 PDF 1.43 MB https://publications.gc.ca/collections/collection_2024/rddc-drdc/DR52-7-3-1971-eng.pdf DREV-TN-2048-72