Engineering:Vesta (rocket): Difference between revisions

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{{Short description|1960s French sounding rocket}}
{{Short description|1960s French sounding rocket}}
{{Infobox rocket|name=Vesta|image=Vesta french sounding rocket.jpg|caption=Vesta 1|height=10.2 m|mass=5.1 tons|stages=1|country-origin=France|derivatives=|sites=CIEES, [[Organization:Guiana Space Centre|Guiana Space Centre]]|stage1thrust=160 kN|payload=500 Kg|diameter=1 m|alt-height=|status=}}The '''Vesta''' sounding rocket, conceived in 1962 by the Laboratoire de recherches balistiques et aérodynamiques (LRBA), a specialized French Army research facility focused on liquid-propelled rocket development.<ref name=":02">{{Cite web |last=Serra |first=Jean-Jacques |date=2008-06-14 |title=Veronique and Vesta |url=http://fuseurop.univ-perp.fr/lrba_e.htm |archive-url=https://web.archive.org/web/20071020121341/http://fuseurop.univ-perp.fr/lrba_e.htm |archive-date=2007-10-20 |access-date=2023-08-26 |website=Rockets in Europe}}</ref><ref name=":1">{{Cite web |last=Capdevila |first=Didier |title=CHRONOLOGIE ARIANE » VERONIQUE ET VESTA |url=http://www.capcomespace.net/dossiers/espace_europeen/espace_francais/veronique_vesta.htm |access-date=2023-08-26 |website=Capcom Espace}}</ref><ref name=":2">{{Cite web |title=Vesta |url=http://astronautix.com/v/vesta.html |access-date=2023-08-26 |website=astronautix.com}}</ref> The initial letter "V" in its name is derived from the city of Vernon.
{{Infobox rocket|name=Vesta|image=Vesta french sounding rocket.jpg|caption=Vesta 1|height=10.2 m|mass=5.1 tons|stages=1|country-origin=France|derivatives=|sites=CIEES, [[Organization:Guiana Space Centre|Guiana Space Centre]]|stage1thrust=160 kN|payload=500 Kg|diameter=1 m|alt-height=|status=}}The '''Vesta''' sounding rocket, conceived in 1962 by the ''Laboratoire de Recherches Balistiques et Aérodynamiques'' (LRBA), a specialized French Army research facility focused on liquid-propelled rocket development.<ref name=":02">{{Cite web |last=Serra |first=Jean-Jacques |date=2008-06-14 |title=Veronique and Vesta |url=http://fuseurop.univ-perp.fr/lrba_e.htm |archive-url=https://web.archive.org/web/20071020121341/http://fuseurop.univ-perp.fr/lrba_e.htm |archive-date=2007-10-20 |access-date=2023-08-26 |website=Rockets in Europe}}</ref><ref name=":1">{{Cite web |last=Capdevila |first=Didier |title=CHRONOLOGIE ARIANE » VERONIQUE ET VESTA |url=http://www.capcomespace.net/dossiers/espace_europeen/espace_francais/veronique_vesta.htm |access-date=2023-08-26 |website=Capcom Espace}}</ref><ref name=":2">{{Cite web |last=Wade |first=Mark |title=Vesta |url=http://astronautix.com/v/vesta.html |access-date=2023-08-26 |website=astronautix.com}}</ref> The initial letter "V" in its name is derived from the city of Vernon.


It was the outcome of an initiative by [[Organization:CNES|CNES]] with the purpose of enabling transportation of more substantial experiments to greater altitudes than the Véronique sounding rocket, also created by the LRBA and in active service at the time.<ref name=":02" /><ref name=":1" />
It was the outcome of an initiative by [[Organization:CNES|CNES]] with the purpose of enabling transportation of more substantial experiments to greater altitudes than the Véronique sounding rocket, also created by the LRBA and in active service at the time.<ref name=":02" /><ref name=":1" />
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== Technical details ==
== Technical details ==
[[File:CNES Vesta rockets.png|thumb|Vesta rockets|left|200x200px]]
[[File:CNES Vesta rockets.png|thumb|Vesta rockets|left|200x200px]]
Operated by a 160&nbsp;kN thrust engine using a combination of [[Chemistry:Nitric acid|nitric acid]] and [[Chemistry:Turpentine|turpentine]] as propellants, the Vesta rocket was 10.2 meters tall with a diameter of 1 meter.<ref name=":2" /><ref>{{Cite web |title=Vesta-1 |url=http://astronautix.com/v/vesta-1.html |access-date=2023-08-26 |website=astronautix.com}}</ref> Weighing 5.1 tons excluding its payload, Vesta had the capability to send a 500&nbsp;kg to an altitude of 400&nbsp;km.<ref name=":02" /><ref name=":1" /><ref name=":2" />
Operated by a 160&nbsp;kN thrust engine using a combination of [[Chemistry:Nitric acid|nitric acid]] and [[Chemistry:Turpentine|turpentine]] as propellants, the Vesta rocket was 10.2 meters tall with a diameter of 1 meter.<ref name=":2" /><ref>{{Cite web |last=Wade |first=Mark |title=Vesta-1 |url=http://astronautix.com/v/vesta-1.html |access-date=2023-08-26 |website=astronautix.com}}</ref> Weighing 5.1 tons excluding its payload, Vesta had the capability to send a 500&nbsp;kg to an altitude of 400&nbsp;km.<ref name=":02" /><ref name=":1" /><ref name=":2" />


== Launches ==
== Launches ==
Between 1965 and 1969 a total of five Vesta rockets were launched.<ref name=":0">{{Cite web |last=Gunter D. |first=Krebs |title=Vesta |url=https://space.skyrocket.de/doc_lau/vesta.htm |access-date=2023-08-26 |website=Gunter's Space Page |language=en}}</ref> These launches took place from both CIEES and [[Organization:Guiana Space Centre|Kourou]].<ref name=":02" /><ref name=":1" /><ref name=":2" /><ref name=":0" /> The first two launches primarily served as validation tests for the rocket's operation,<ref name=":02" /> whereas the subsequent three carried out scientific experiments.<ref name=":1" /><ref name=":2" />
Between 1965 and 1969 a total of five Vesta rockets were launched.<ref name=":0">{{Cite web |last=Krebs |first=Gunter D. |title=Vesta |url=https://space.skyrocket.de/doc_lau/vesta.htm |access-date=2023-08-26 |website=Gunter's Space Page |language=en}}</ref> These launches took place from both CIEES and [[Organization:Guiana Space Centre|Kourou]].<ref name=":02" /><ref name=":1" /><ref name=":2" /><ref name=":0" /> The first two launches primarily served as validation tests for the rocket's operation,<ref name=":02" /> whereas the subsequent three carried out scientific experiments.<ref name=":1" /><ref name=":2" />


A pig-tailed macaque named ''Martine'' was launched on March 7, 1967, and another named ''Pierette'' on March 13.<ref name=":1" /> These suborbital flights reached {{convert|243|km|mi|abbr=on}} and {{convert|234|km|mi|abbr=on}}, respectively. Martine became the first monkey to survive more than a couple of hours after flying above the international definition of the edge of space. ([[Astronomy:Ham (chimpanzee)|Ham]] and [[Engineering:Enos (chimpanzee)|Enos]], launched earlier by the United States, were chimpanzees).<ref>Burgess & Dubbs (2007), p. 387.</ref>
A pig-tailed macaque named ''Martine'' was launched on March 7, 1967, and another named ''Pierette'' on March 13.<ref name=":1" /> These suborbital flights reached {{convert|243|km|mi|abbr=on}} and {{convert|234|km|mi|abbr=on}}, respectively. Martine became the first monkey to survive more than a couple of hours after flying above the international definition of the edge of space. ([[Astronomy:Ham (chimpanzee)|Ham]] and [[Engineering:Enos (chimpanzee)|Enos]], launched earlier by the United States, were chimpanzees).<ref>{{Cite book |last=Burgess |first=Colin |url=https://archive.org/details/Animalsinspace |title=Animals in Space: From Research Rockets to the Space Shuttle |last2=Dubbs |first2=Chris |date=2007 |publisher=Springer |isbn=978-0-387-49678-8 |series=Physics and Astronomy |location=New York |page=[https://archive.org/details/Animalsinspace/page/n420 387] |doi=10.1007/978-0-387-49678-8}}</ref>
{| class="wikitable sortable"
{| class="wikitable sortable"
|+Vesta launches<ref name=":02" /><ref name=":1" /><ref name=":2" /><ref name=":0" />
|+Vesta launches<ref name=":02" /><ref name=":1" /><ref name=":2" /><ref name=":0" />
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|FU123 Technology
|FU123 Technology
|187&nbsp;km
|187&nbsp;km
|Success
|{{Success}}
|-
|-
|25 October  1965
|25 October  1965
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|FU123 Technology
|FU123 Technology
|109&nbsp;km
|109&nbsp;km
|Partial success
|{{Partial success}}
|-
|-
|7 March 1967
|7 March 1967
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|FU147 Biology
|FU147 Biology
|243&nbsp;km
|243&nbsp;km
|Success
|{{Success}}
|-
|-
|13 March 1967
|13 March 1967
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|FU147 Biology
|FU147 Biology
|234&nbsp;km
|234&nbsp;km
|Success
|{{Success}}
|-
|-
|8 November 1969
|8 November 1969
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|FU189 Astronomy
|FU189 Astronomy
|204&nbsp;km
|204&nbsp;km
|Partial success
|{{Partial success}}
|}
|}


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== References ==
== References ==
{{Reflist}}
{{Reflist}}{{French rockets}}
 
[[Category:Experimental rockets]]
[[Category:Experimental rockets]]


{{Sourceattribution|Vesta (rocket)}}
{{Sourceattribution|Vesta (rocket)}}

Latest revision as of 02:31, 16 July 2025

Short description: 1960s French sounding rocket
Vesta
Vesta french sounding rocket.jpg
Vesta 1
Country of originFrance
Size
Height10.2 m
Diameter1 m
Mass5.1 tons
Stages1
Capacity
Launch history
Launch sitesCIEES, Guiana Space Centre
First stage
Thrust160 kN

The Vesta sounding rocket, conceived in 1962 by the Laboratoire de Recherches Balistiques et Aérodynamiques (LRBA), a specialized French Army research facility focused on liquid-propelled rocket development.[1][2][3] The initial letter "V" in its name is derived from the city of Vernon.

It was the outcome of an initiative by CNES with the purpose of enabling transportation of more substantial experiments to greater altitudes than the Véronique sounding rocket, also created by the LRBA and in active service at the time.[1][2]

Technical details

Vesta rockets

Operated by a 160 kN thrust engine using a combination of nitric acid and turpentine as propellants, the Vesta rocket was 10.2 meters tall with a diameter of 1 meter.[3][4] Weighing 5.1 tons excluding its payload, Vesta had the capability to send a 500 kg to an altitude of 400 km.[1][2][3]

Launches

Between 1965 and 1969 a total of five Vesta rockets were launched.[5] These launches took place from both CIEES and Kourou.[1][2][3][5] The first two launches primarily served as validation tests for the rocket's operation,[1] whereas the subsequent three carried out scientific experiments.[2][3]

A pig-tailed macaque named Martine was launched on March 7, 1967, and another named Pierette on March 13.[2] These suborbital flights reached 243 km (151 mi) and 234 km (145 mi), respectively. Martine became the first monkey to survive more than a couple of hours after flying above the international definition of the edge of space. (Ham and Enos, launched earlier by the United States, were chimpanzees).[6]

Vesta launches[1][2][3][5]
Date Site Vehicle Mission Apogee Results
15 October 1965 CIEES Vesta 01 FU123 Technology 187 km Success
25 October 1965 CIEES Vesta 03 FU123 Technology 109 km Partial success
7 March 1967 CIEES Vesta 04 FU147 Biology 243 km Success
13 March 1967 CIEES Vesta 05 FU147 Biology 234 km Success
8 November 1969 Kourou Vesta 02 FU189 Astronomy 204 km Partial success

See also

  • French space program
  • Véronique
  • Diamant

References

Template:French rockets