000	02077nam  2200397zi 4500
001	9.927698
003	CaOODSP
005	20231003072910
006	m     o  d f
007	cr |n|||||||||
008	230921e198109uuabcad   o    f000 0 eng d
040	|aCaOODSP|beng|erda|cCaOODSP
043	|an-cn-ab
086	1 |aDR52-6/8-1981E-PDF
100	1 |aSchilling, K., |eauthor.
245	12|aA winged rocket boosted target (ROBOT-X) (U) / |cby K. Schilling.
264	1|aRalston, Alberta : |bDefence Research Establishment Suffield, |cSeptember, 1981.
300	|a1 online resource (iv, [9] pages, 16 unnumbered pages) : |billustrations, charts
336	|atext|btxt|2rdacontent
337	|acomputer|bc|2rdamedia
338	|aonline resource|bcr|2rdacarrier
490	1 |aSuffield memorandum ; |vno. 1062
500	|a"PCN 21V10"--title page.
500	|aPDF is missing page 9 and figures 8, 9, and 14.
500	|aDigitized edition from print [produced by Defence Research and Development Canada].
520	3 |a"A winged rocket boosted target (ROBOT-X) is proposed as an inexpensive alternative to turbine engine driven drones for low level/high speed target simulation missions. The basic configuration of a ROBOT-X using 19 CRV7 rocket motors for propulsion is described, results of performance estimates are presented, and the feasibility of ROBOT-X for the target missions mentioned above is demonstrated"--abstract.
650	0|aGuided missiles|xPropulsion systems|xDesign and construction.
650	0|aCruise missiles|zCanada|xCost of operation.
650	6|aMissiles|xSystèmes de propulsion|xConception et construction.
650	6|aMissiles de croisière|zCanada|xFrais d'exploitation.
655	7|aTechnical reports|2lcgft
655	7|aRapports techniques|2rvmgf
710	2 |aDefence Research Establishment Suffield, |eissuing body.
830	#0|aSuffield memorandum ;|vno. 1062.|w(CaOODSP)9.926310
856	40|qPDF|s699 KB|uhttps://publications.gc.ca/collections/collection_2023/rddc-drdc/DR52-6-8-1981-eng.pdf