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to orbit. In June 1969, the Space and
Missile Systems Organization (SAMSO) began development of the Burner IIA configuration which would offer a tandem motor injection capability and almost twice the capability of Burner II. In June 1971, the last of the Burner II missions was launched from Vandenberg by a Thor/Burner II launch vehicle and carried an SESP-1 space environmental satellite.
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In
September 1965, Air Force Space Systems Division announced the development of a new, low cost upper stage called Burner II. It was intended as the smallest maneuverable upper stage in the Air Force inventory. In June 1967, the first Thor/Burner II vehicle successfully launched a pair of satellites
70:
rockets. Atlas E/F vehicles were configured with a Burner II/IIA stage and launched in 1968 and 1972. The first launch failed with the second delivering a radiation research payload for the Space Test
Program (P72-1 Radsat) using Burner IIA.
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In the mid-1970s Burner II was also studied for use as an upper stage in combination with the Space
Shuttle. NASA managers choose other solutions for missions where upper stages were required.
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and was derived from the fourth stage of the Scout launch vehicle. The Burner 2 stage was powered by a
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Weyers, Vernon J.; Sagerman, Gary D.; Borsody, Janos; Lubick, Robert J. (June 1974).
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In addition to use on Delta family rockets, Burner 2 stages have been used on both
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Comparative
Evaluation of Existing Expendable Upper Stages for Space Shuttle
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Space and
Missile Systems Organization, A Chronology, 1954-1979
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To Reach the High
Frontier: A History of U.S. Launch Vehicles
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194:"The Atlas E/F Launch Vehicle - An Unsung Workhorse"
47:since 1965. The Burner 1 stage was also called the
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128:(Report). Defense Technical Information Center
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201:Journal of the British Interplanetary Society
91:Launius, Roger D.; Dennis R. Jenkins (2002).
16:Rocket stage which can be used as a space tug
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192:Powell, J.W.; Richards, G.R. (1991).
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35:have been used as upper stages of
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363:Advanced Cryogenic Evolved Stage
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147:White, J. Terry (June 4, 2012).
233:(Report). NASA NTRS. p. 9
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511:. You can help Knowledge by
99:University Press of Kentucky
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507:This rocketry article is a
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175:Encyclopedia Astronautica
368:Exploration Upper Stage
151:. White Eagle Aerospace
149:"Thor Burner II Finale"
464:Payload Assist Module
563:Thor (rocket family)
479:Transfer Orbit Stage
454:Inertial Upper Stage
181:on October 16, 2008.
101:. pp. 186–213.
55:solid rocket motor.
573:1971 in spaceflight
568:1967 in spaceflight
213:1991JBIS...44..229P
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513:expanding it
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334:Star 27 / 37
280:Upper stages
235:. Retrieved
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179:the original
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130:. Retrieved
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49:Altair stage
39:such as the
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237:December 3,
207:: 229–240.
155:December 3,
132:December 3,
41:Thor-Burner
552:Categories
474:Saturn IVB
108:0813127211
78:References
29:Burner IIA
484:Transtage
469:Saturn IV
347:Yuanzheng
314:CTS / SMA
304:Castor 30
171:"Star 37"
25:Burner II
409:Blok 2BL
434:Delta-P
429:Delta-K
424:Delta-D
382:Retired
356:Planned
309:Centaur
209:Bibcode
53:Star 37
31:rocket
419:Burner
414:Blok D
404:Astris
399:Altair
329:Fregat
287:Active
105:
33:stages
27:, and
21:Burner
459:KVD-1
444:FG-02
389:Agena
342:Volga
324:DM-03
231:(PDF)
197:(PDF)
126:(PDF)
68:Titan
64:Atlas
45:Delta
509:stub
449:Ikar
439:EPKM
394:Able
373:KVTK
337:/ 48
319:DCSS
299:Briz
294:AVUM
239:2022
157:2022
134:2022
103:ISBN
66:and
43:and
19:The
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23:,
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