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- Zenit ist die Bezeichnung für eine von Oerlikon Contraves in der Schweiz entwickelte Höhenforschungsrakete, die unter anderem der Erforschung der Ionosphäre diente. (de)
- Zenit-C was a sounding rocket developed from Oerlikon Contraves (today Rheinmetall Air Defence in Switzerland. The Zenit was a single-step rocket with a length of 5.6 meters, a diameter of 0.42 meter and a takeoff weight of 610 kilograms. Propelled by a solid-propellant engine which supplied a thrust between 45 kN at launch and 22 kN in flight, the Zenit could carry a payload of 25 kilograms to a height of 210 km or a payload of 130 kilograms to a height of 115 km. At its maiden flight on October 27, 1967, at Salto di Quirra the Zenit topped 145 km. The Zenit was later launched only twice — once on July 30, 1971, at Salto di Quirra with a British rocket as a starting stage and once on December 13, 1973, at Andøya likewise with a "Cuckoo" starting stage. Oerlikon used the knowledge from the Ground to Air Missile RSE Kriens for the Zenit. (en)
- Zenit-C, foi um foguete de sondagem de origem suíça. Esse foguete usava o motor do míssil Micon, desenvolvidopelas empresas: Oerlikon-Bührle Machine Tools Co e Contraves AG, desde 1947. No final da década de 60, esse motor foi usado no foguete Zenit.Com apenas três lançamentos, nos últimos dois, foi usado o motor Cuckoo de origem inglesa, como primeiro estágio. (pt)
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- Zenit ist die Bezeichnung für eine von Oerlikon Contraves in der Schweiz entwickelte Höhenforschungsrakete, die unter anderem der Erforschung der Ionosphäre diente. (de)
- Zenit-C, foi um foguete de sondagem de origem suíça. Esse foguete usava o motor do míssil Micon, desenvolvidopelas empresas: Oerlikon-Bührle Machine Tools Co e Contraves AG, desde 1947. No final da década de 60, esse motor foi usado no foguete Zenit.Com apenas três lançamentos, nos últimos dois, foi usado o motor Cuckoo de origem inglesa, como primeiro estágio. (pt)
- Zenit-C was a sounding rocket developed from Oerlikon Contraves (today Rheinmetall Air Defence in Switzerland. The Zenit was a single-step rocket with a length of 5.6 meters, a diameter of 0.42 meter and a takeoff weight of 610 kilograms. Propelled by a solid-propellant engine which supplied a thrust between 45 kN at launch and 22 kN in flight, the Zenit could carry a payload of 25 kilograms to a height of 210 km or a payload of 130 kilograms to a height of 115 km. At its maiden flight on October 27, 1967, at Salto di Quirra the Zenit topped 145 km. The Zenit was later launched only twice — once on July 30, 1971, at Salto di Quirra with a British rocket as a starting stage and once on December 13, 1973, at Andøya likewise with a "Cuckoo" starting stage. Oerlikon used the knowledge from th (en)
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- Zenit (Höhenforschungsrakete) (de)
- Zenit-C (pt)
- Zenit-C (en)
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