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- VS-40 diameter "1.01".
- VS-40 height "9500.0".
- VS-40 mass "6800.0".
- VS-40 lowerEarthOrbitPayload "500.0".
- VS-40 mass "6800.0".
- VS-40 abstract "The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel, stabilized aerodynamically, distributed between the first stage S40TM (4,200 kg) engine and the second stage S44M (810 kg) engine.This configuration corresponds to the upper stages of the VLS-1 rocket.".
- VS-40 countryOrigin Brazil.
- VS-40 diameter "1.01".
- VS-40 failedLaunches "0".
- VS-40 height "9.5".
- VS-40 launchSite Alc%C3%A2ntara_Launch_Center.
- VS-40 launchSite And%C3%B8ya_Rocket_Range.
- VS-40 lowerEarthOrbitPayload "500000.0".
- VS-40 maidenFlight "1993-04-02".
- VS-40 manufacturer Instituto_de_Aeron%C3%A1utica_e_Espa%C3%A7o.
- VS-40 mass "6800000.0".
- VS-40 rocketFunction Sounding_rocket.
- VS-40 rocketStages "2".
- VS-40 status "Active".
- VS-40 thumbnail Foguete_VS_40.jpg?width=300.
- VS-40 totalLaunches "3".
- VS-40 wikiPageExternalLink indexx.php?secao=lancadores.
- VS-40 wikiPageExternalLink 7407479734.
- VS-40 wikiPageExternalLink ?action=vs40.
- VS-40 wikiPageID "24548387".
- VS-40 wikiPageRevisionID "543354159".
- VS-40 altDiameter "3.31".
- VS-40 altHeight "31.1".
- VS-40 altLeo "650.0".
- VS-40 altMass "14900.0".
- VS-40 altStage1thrust "46848".
- VS-40 caption "VS-40 rocket on display in Brasília".
- VS-40 countryOrigin Brazil.
- VS-40 diameter "1.01 m".
- VS-40 fail "0".
- VS-40 first "1993-04-02".
- VS-40 function Sounding_rocket.
- VS-40 hasPhotoCollection VS-40.
- VS-40 height "9.50 m".
- VS-40 imsize "240".
- VS-40 launches "3".
- VS-40 leoPayload "500.0".
- VS-40 manufacturer Instituto_de_Aeronáutica_e_Espaço.
- VS-40 mass "6800.0".
- VS-40 name "VS-40".
- VS-40 sites Andøya_Rocket_Range.
- VS-40 sites Centro_de_Lançamento_de_Alcântara.
- VS-40 stage1engines "1".
- VS-40 stage1fuel Solid-fuel_rocket.
- VS-40 stage1name "S40TM".
- VS-40 stage1si "275.0".
- VS-40 stage1thrust "208.39 kN".
- VS-40 stage1time "56.0".
- VS-40 stage2engines "1".
- VS-40 stage2fuel Solid-fuel_rocket.
- VS-40 stage2name "S44M".
- VS-40 stage2si "282.0".
- VS-40 stage2thrust "33.24 kN".
- VS-40 stage2time "68.0".
- VS-40 stages "2".
- VS-40 status "Active".
- VS-40 subject Category:Sounding_rockets_of_Brazil.
- VS-40 subject Category:Space_program_of_Brazil.
- VS-40 type MeanOfTransportation.
- VS-40 type Rocket.
- VS-40 type DesignedArtifact.
- VS-40 comment "The VS-40 (Foguete Suborbital VS-40) is a Brazilian sounding rocket using solid fuel, stabilized aerodynamically, distributed between the first stage S40TM (4,200 kg) engine and the second stage S44M (810 kg) engine.This configuration corresponds to the upper stages of the VLS-1 rocket.".
- VS-40 label "VS-40".
- VS-40 label "VS-40".
- VS-40 label "VS-40".
- VS-40 sameAs VS-40.
- VS-40 sameAs VS-40.
- VS-40 sameAs m.080mw51.
- VS-40 sameAs Q5955968.
- VS-40 sameAs Q5955968.
- VS-40 wasDerivedFrom VS-40?oldid=543354159.
- VS-40 depiction Foguete_VS_40.jpg.
- VS-40 isPrimaryTopicOf VS-40.
- VS-40 name "VS-40 (Foguete Suborbital VS-40)".