31:
299:
itself with technical challenges involved in the missile's development. Accordingly, the program was extended, with some of the Army's requirements being relaxed; however, in
September 1958 the program was determined to be too far behind schedule and too far over budget to be successful, and the contract for the Dart was cancelled. The Army adopted the SS.10, designated MGM-21, and the
298:
The first launch trials of the XSSM-A-23 prototype missiles took place in August 1954; over the next year, forty additional tests took place. These proved less than satisfactory; by 1957, the Dart was still not ready for service, and it was believed that
Aerophysics Development had overextended
235:
missile being developed in France. After evaluating the SS.10 in 1952–53, the Army issued a contract for the full development of the
Aerophysics Development missile, designated SSM-A-23 Dart, in April 1953.
1180:
224:
1049:
1039:
1175:
1185:
1014:
264:
1004:
612:
543:
524:
445:
499:. Study of the Subcommittee on Patents, Trademarks, and Copyrights. Washington. D.C.: Government Printing Office.
260:
169:
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605:
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283:
271:
that spooled from the missile during flight. Due to difficulties experienced in testing to ensure accuracy, an
256:
252:
598:
192:
248:
571:
383:
259:
designated T149; helicopter launching was also considered as a possibility. Guidance was by
239:
The SSM-A-23 was of conventional configuration for an anti-tank missile of the time, having
290:
then acquired the company as part of a larger deal with
Studebaker-Packard in August 1956.
8:
268:
228:
199:
in the 1950s. After protracted development, the missile, similar in design to the French
215:
The initial requirement for a guided anti-tank missile, intended for the replacement of
1140:
621:
196:
67:
576:
Directory of U.S. Military
Rockets and Missiles, Appendix 1: Early Missiles and Drones
303:, designated AGM-22, in its stead. The program had cost $ 44 million in 1955 dollars.
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512:
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453:
282:
During the development of the Dart, Aerophysics
Development was acquired by the
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in the tail of the missile and guiding the missile to the target with commands
255:
provided thrust. The launcher for the missile was mounted on a variant of the
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903:
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30:
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223:
in the role, was issued by the U.S. Army in 1951; that
November, the
1181:
Abandoned military rocket and missile projects of the United States
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1104:
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1059:
1054:
1044:
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994:
989:
220:
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was proposed for terminal homing. The missile was fitted with a
1135:
497:
The
Research and Development Factor in Mergers and Acquisitions
300:
232:
204:
200:
533:
517:
Bradley: A History of
American Fighting and Support Vehicles
152:
552:
279:
warhead intended to defeat the armor of enemy tanks.
553:Ordway, Frederick Ira; Ronald C. Wakeford (1960).
1167:
534:Jacobs, Horace; Eunice Engelke Whitney (1962).
1176:Anti-tank guided missiles of the United States
286:, the purchase taking place in December 1954.
231:, similar in concept and configuration to the
606:
538:. New York: Springer Science+Business Media.
147:3,333 yd (1.894 mi; 3.048 km)
480:The Handbook of Rockets and Guided Missiles
203:, was cancelled in favor of purchasing the
157:900 ft/s (610 mph; 990 km/h)
613:
599:
555:International Missile and Spacecraft Guide
1186:Anti-tank guided missiles of the Cold War
624:missile and rocket designations 1948–1963
511:
210:
494:
572:"Aerophysics Development SSM-A-23 Dart"
1168:
569:
477:
378:
376:
374:
372:
370:
293:
594:
536:Missile and Space Projects Guide 1962
360:
358:
356:
354:
390:. United States Army. 4 October 2016
344:
342:
340:
338:
328:
326:
324:
322:
320:
180:Parsch 2003, Jacobs and Whitney 1962
570:Parsch, Andreas (2 February 2003).
367:
263:, the missile operator following a
225:Aerophysics Development Corporation
13:
401:
351:
14:
1197:
335:
317:
247:providing control; a dual-thrust
243:wings and stabilizing fins, with
106:3 ft 4 in (1.02 m)
443:
364:Ordway and Wakeford 1960, p.USA4
227:responded with a proposal for a
29:
470:
261:manual command to line of sight
170:Manual command to line of sight
519:. Novato, CA: Presidio Press.
482:. Chicago: Perastadion Press.
437:
428:
419:
410:
348:Jacobs and Whitney 1962, p.44.
284:Studebaker-Packard Corporation
1:
306:
257:M59 armored personnel carrier
127:Dual-thrust solid-fuel rocket
495:Friedman, Murray N. (1958).
478:Bowman, Norman John (1957).
253:Grand Central Rocket Company
7:
978:Unguided rockets, 1940–1963
10:
1202:
74:Specifications (XSSM-A-23)
1149:
1123:
977:
871:
725:
629:
557:. New York: McGraw-Hill.
450:Encyclopedia Astronautica
388:White Sands Missile Range
175:
161:
151:
139:
131:
123:
118:
110:
102:
94:
86:
78:
73:
63:
58:
51:Place of origin
50:
40:
28:
21:
872:1955–1963 missile system
726:1951–1955 missile system
630:1948–1951 missile system
311:
193:anti-tank-guided missile
82:100 lb (45 kg)
249:solid-propellant rocket
98:8 in (200 mm)
90:5 ft (150 cm)
407:Hunnicutt 1999, p.176.
211:Design and development
1156:Designation uncertain
578:. Designation-Systems
434:Friedman 1958, p. 20.
416:Hunnicutt 1999, p.78.
456:on December 28, 2016
425:Bowman 1957, p.102.
294:Operational history
229:wire-guided missile
35:XSSM-A-23 prototype
1124:Undesignated types
622:United States Army
197:United States Army
195:developed for the
68:United States Army
1163:
1162:
545:978-1-4899-6967-5
217:recoilless rifles
185:
184:
181:
45:Anti-tank missile
16:Anti-tank missile
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452:. Archived from
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251:produced by the
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513:Hunnicutt, R.P.
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273:infrared seeker
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59:Service history
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12:
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5:
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526:978-0891416944
525:
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492:
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446:"Dart missile"
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288:Curtiss-Wright
269:sent by a wire
212:
209:
189:XSSM-A-23 Dart
183:
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153:Maximum speed
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26:
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23:SSM-A-23 Dart
15:
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277:shaped charge
274:
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114:Shaped charge
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57:
54:United States
53:
49:
46:
43:
39:
32:
27:
20:
1153:Not assigned
842:
580:. Retrieved
575:
554:
535:
516:
496:
479:
471:Bibliography
458:. Retrieved
454:the original
449:
444:Wade, Mark.
439:
430:
421:
412:
403:
392:. Retrieved
387:
297:
281:
265:sodium flare
238:
214:
188:
186:
64:Used by
332:Parsch 2003
141:Operational
1170:Categories
582:2017-12-08
563:B000MAEGVC
505:B0007FC10K
488:B0007EC5N4
460:2017-12-08
394:2017-12-08
307:References
245:spoilerons
176:References
135:Solid fuel
132:Propellant
1141:Ping-Pong
241:cruciform
207:missile.
863:SSM-A-27
853:SAM-A-25
843:SSM-A-23
823:SAM-A-19
818:SAM-A-18
813:SSM-A-17
808:SSM-A-16
803:SSM-A-15
798:SSM-A-14
793:SSM-A-13
788:SSM-A-12
717:SSM-G-17
712:SSM-G-16
707:SSM-G-15
702:SSM-G-14
697:SSM-G-13
692:SSM-G-12
682:RTV-G-10
515:(1999).
221:Bazookas
163:Guidance
103:Wingspan
95:Diameter
1131:Dervish
838:RV-A-22
778:RV-A-10
773:SSM-A-9
763:SAM-A-7
677:SSM-G-9
672:SSM-G-8
667:SAM-G-7
662:RTV-G-6
657:CTV-G-5
652:RTV-G-4
647:RTV-G-3
642:RTV-G-2
637:RTV-G-1
191:was an
111:Warhead
1136:Lobber
768:RV-A-8
758:RV-A-6
753:RV-A-5
748:RV-A-4
743:RV-A-3
738:RV-A-2
733:RV-A-1
561:
542:
523:
503:
486:
384:"Dart"
165:system
124:Engine
87:Length
312:Notes
301:SS.11
233:SS.10
205:SS.11
201:SS.10
143:range
858:A-26
848:A-24
833:A-21
828:A-20
783:G-11
687:G-11
559:ASIN
540:ISBN
521:ISBN
501:ASIN
484:ASIN
219:and
187:The
79:Mass
41:Type
1115:M74
1110:M73
1105:M72
1100:M61
1095:M60
1090:M55
1085:M51
1080:M50
1075:M47
1070:M31
1065:M30
1060:M29
1055:M28
1050:M27
1045:M26
1040:M25
1035:M21
1030:M20
1025:M17
1020:M16
1015:M12
1010:M10
969:M19
964:M18
959:M17
954:M16
949:M15
944:M14
939:M13
934:M12
929:M11
924:M10
1172::
1005:M9
1000:M8
995:M7
990:M6
985:M2
919:M9
914:M8
909:M7
904:M6
899:M5
894:M4
889:M3
884:M2
879:M1
574:.
448:.
386:.
369:^
353:^
337:^
319:^
614:e
607:t
600:v
585:.
565:.
548:.
529:.
507:.
490:.
463:.
397:.
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.