| 词条 | Mélanie (rocket) |
| 释义 |
It had a thrust increasing from 6.2 kN (Monica I) to 8.2 kN (Monica V) and a burn time of about five seconds. Melanie was later used in several ATEF and ONERA rockets. In the ONERA rockets, such as Daniel, Antares and Berenice, Melanie was placed inside a 22 cm diameter cylindrical housing. This version delivered a total impulse of 48 kN.s with about 22 kilograms of propellant. References1. ^Les débuts de la recherche spatiale française IFHE,, Institut français d'histoire de l'espace - 2007 "Caractéristiques des fusées météo à propulsion solide et propulsion hybride.... Mélanie" External links
1 : Rockets and missiles |
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