Rockair: Difference between revisions
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{{Infobox spaceflight |
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{{Dictionary|date= June 2019}} |
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| name = Rockair (or "Rockaire") |
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| image = Deacon Rockoon.jpg |
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| image_caption = A Deacon rocket, in this case being used as a [[Rockoon]]. The Rockoon concept later succeeded the Rockair, however, note that no balloon was involved in Rockair launches. |
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| image_alt = Deacon rocket suspended from a balloon as a part of a Rockoon lanch |
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| mission_type = Research |
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| operator = [[United States Navy]] and [[United States Air Force|Air Force]] |
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| mission_duration = 491 days |
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| manufacturer = [[North American Aviation]] and [[Allegany Ballistics Laboratory]] |
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}} |
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The '''Rockair''' was first suggested by [[Hermann Oberth]] in his 1929 book ''[[Wege zur Raumschiffahrt]]''.<ref name=":0">{{Cite web |last=Corliss |first=William |date=1971 |title=NASA Sounding Rockets, 1958-1968, A Historical Summary |url=https://www.nasa.gov/wp-content/uploads/2023/03/sp-4401.pdf |access-date=March 2, 2024 |website=NASA}}</ref> Rockair concepts were developed by both the [[United States Air Force]] and [[United States Navy|Navy]], both generally finding marginal use in the concept.<ref name=":0" /> The Air Force began studying the concept of an air-launched sounding rocket in 1947, while the Navy managed to get the first launch on August 16, 1955, using an [[McDonnell F2H Banshee|F2H2]] off of [[Wallops Island]]. The [[Folding-Fin Aerial Rocket|folded-fin aerial rocket]](FFAR)<ref name=":0" /><ref>{{Cite web |title=FFAR |url=http://www.astronautix.com/f/ffar.html |access-date=2024-03-02 |website=www.astronautix.com}}</ref> reached an altitude of 54,864 m (180,000 ft). The Air Force followed up with their first air-launched sounding rocket concept on December 13, 1956, under the name "Rockaire".<ref>{{Cite web |title=Rockaire |url=http://www.astronautix.com/r/rockaire.html |access-date=2024-03-02 |website=www.astronautix.com}}</ref> A [[Deacon (rocket)|Deacon]] rocket was used, launched from a [[North American F-86 Sabre|F-86 fighter aircraft]]. |
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'''Rockair''' was a United States [[sounding rocket]] designed for launch from an airplane, which was tested 1955. The Rockair had a maximum height of 50 km (160,000 ft), a takeoff thrust of 3.00 kN (675 lbf), a diameter of {{convert|70|mm|in|frac=8|abbr=on}} and a length of {{convert|1.20|m|in|abbr=on}}. |
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The Navy Rockair had a total of 5 launches, while the Air Force Rockaire had a total of 4 for a combined 9 launches. |
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==External links== |
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*https://web.archive.org/web/20050212235252/http://astronautix.com/lvs/rockair.htm |
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According to a NASA historical summary,<ref name=":0" /> no important scientific research was every carried out with the Rockair concept. It had very little popularity, in contrast to the "Rockoon" which was launched in the hundreds during the 1950s. |
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⚫ | |||
== Launch History of the Rockair == |
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{| class="wikitable" |
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|+ |
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!Date |
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!Launch Site |
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!Rocket |
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!Launch Platform |
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!Apogee |
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|- |
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|August 16, 1955 |
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|[[Naval Aviation Ordnance Test Station|NAOTS]] |
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|[[Folding-Fin Aerial Rocket|FFAR]] |
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|[[McDonnell F2H Banshee|F2H2]] |
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|50 km(31 mi) |
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|- |
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|August 16, 1955 |
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|[[Naval Aviation Ordnance Test Station|NAOTS]] |
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|[[Folding-Fin Aerial Rocket|FFAR]] |
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|[[McDonnell F2H Banshee|F2H2]] |
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|55 km(34 mi) |
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|- |
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|August 16, 1955 |
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|[[Naval Aviation Ordnance Test Station|NAOTS]] |
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|[[Folding-Fin Aerial Rocket|FFAR]] |
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|[[McDonnell F2H Banshee|F2H2]] |
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|9 km(5.5 mi) |
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|- |
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|November 1, 1955 |
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|[[Naval Aviation Ordnance Test Station|NAOTS]] |
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|[[Folding-Fin Aerial Rocket|FFAR]] |
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|[[McDonnell F2H Banshee|F2H2]] |
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|50 km(31 mi) |
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|- |
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|November 1, 1955 |
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|[[Naval Aviation Ordnance Test Station|NAOTS]] |
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|[[Folding-Fin Aerial Rocket|FFAR]] |
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|[[McDonnell F2H Banshee|F2H2]] |
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|50 km(31 mi) |
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|} |
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== Launch History of the Rockaire == |
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{{Rocket-stub}} |
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{| class="wikitable" |
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!Date |
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!Launch Site |
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!Rocket |
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!Launch Platform |
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!Apogee |
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|- |
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|December 13, 1956 |
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|[[Holloman Air Force Base|Holloman]] |
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|[[Deacon (rocket)|Deacon]] |
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|[[North American F-86D Sabre|F-86D]] |
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|44 km(27 mi) |
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|- |
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|December 14, 1956 |
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|[[Holloman Air Force Base|Holloman]] |
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|[[Deacon (rocket)|Deacon]] |
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|[[North American F-86D Sabre|F-86D]] |
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|42 km(26 mi) |
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|- |
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|December 17, 1956 |
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|[[Holloman Air Force Base|Holloman]] |
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|[[Deacon (rocket)|Deacon]] |
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|[[North American F-86D Sabre|F-86D]] |
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|43 km(26 mi) |
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|- |
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|December 19, 1956 |
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|[[Holloman Air Force Base|Holloman]] |
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|[[Deacon (rocket)|Deacon]] |
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|[[North American F-86D Sabre|F-86D]] |
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|45 km(27 mi) |
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|} |
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==References== |
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{{Reflist}} |
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⚫ |
Latest revision as of 15:12, 6 August 2024
Mission type | Research |
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Operator | United States Navy and Air Force |
Mission duration | 491 days |
Spacecraft properties | |
Manufacturer | North American Aviation and Allegany Ballistics Laboratory |
The Rockair was first suggested by Hermann Oberth in his 1929 book Wege zur Raumschiffahrt.[1] Rockair concepts were developed by both the United States Air Force and Navy, both generally finding marginal use in the concept.[1] The Air Force began studying the concept of an air-launched sounding rocket in 1947, while the Navy managed to get the first launch on August 16, 1955, using an F2H2 off of Wallops Island. The folded-fin aerial rocket(FFAR)[1][2] reached an altitude of 54,864 m (180,000 ft). The Air Force followed up with their first air-launched sounding rocket concept on December 13, 1956, under the name "Rockaire".[3] A Deacon rocket was used, launched from a F-86 fighter aircraft.
The Navy Rockair had a total of 5 launches, while the Air Force Rockaire had a total of 4 for a combined 9 launches.
According to a NASA historical summary,[1] no important scientific research was every carried out with the Rockair concept. It had very little popularity, in contrast to the "Rockoon" which was launched in the hundreds during the 1950s.
Launch History of the Rockair
[edit]Date | Launch Site | Rocket | Launch Platform | Apogee |
---|---|---|---|---|
August 16, 1955 | NAOTS | FFAR | F2H2 | 50 km(31 mi) |
August 16, 1955 | NAOTS | FFAR | F2H2 | 55 km(34 mi) |
August 16, 1955 | NAOTS | FFAR | F2H2 | 9 km(5.5 mi) |
November 1, 1955 | NAOTS | FFAR | F2H2 | 50 km(31 mi) |
November 1, 1955 | NAOTS | FFAR | F2H2 | 50 km(31 mi) |
Launch History of the Rockaire
[edit]Date | Launch Site | Rocket | Launch Platform | Apogee |
---|---|---|---|---|
December 13, 1956 | Holloman | Deacon | F-86D | 44 km(27 mi) |
December 14, 1956 | Holloman | Deacon | F-86D | 42 km(26 mi) |
December 17, 1956 | Holloman | Deacon | F-86D | 43 km(26 mi) |
December 19, 1956 | Holloman | Deacon | F-86D | 45 km(27 mi) |
References
[edit]- ^ a b c d Corliss, William (1971). "NASA Sounding Rockets, 1958-1968, A Historical Summary" (PDF). NASA. Retrieved March 2, 2024.
- ^ "FFAR". www.astronautix.com. Retrieved 2024-03-02.
- ^ "Rockaire". www.astronautix.com. Retrieved 2024-03-02.