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    VLM (rocket) - Wikipedia

    The VLM (Veículo Lançador de Microsatélites) is a proposed three-stage satellite launcher being developed by the Brazilian General Command for Aerospace Technology in collaboration with Germany. The project originated in 2008 as a simplified version of the VLS-1 rocket, using only the core stages. … See more

    The VLM-1 vehicle is designed to deliver up to 150 kg (330 lb) to a 300 km equatorial circular orbit. VLM-1 is projected to have a total mass of 28,000 kg (62,000 lb), including 10 tons of propellant. The first two stages will … See more

    Brazilian researchers have studied the possibility of a cost-competitive launch system using S-50 motors in the first two stages and a set of liquid engines in the third stage. This … See more

    Development on VLM started in 2008 for the purpose of low-cost and reliable launch of microsatellites, based on existing Brazilian sounding rockets like the VS-40 and technology … See more

    In the future, the L5 liquid fuel rocket engine will replace the solid 3rd stage engine. The configuration will be:
    • Stage 1: S-50 rocket motor
    • Stage … See more

    Home website of VLM-1 at the Brazilian Space Agency
    • Domingos Zaparolli (January 2022). "Launch remains distant".
    Media related to VLM (rocket) at Wikimedia Commons See more

     
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  3. VS-50 - Wikipedia

  4. VLM (rocket) - Wikiwand

  5. VLS-1 - Wikipedia

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  7. New DLR Team to Focus on VS-50 “Very Heavy Lift” …

    Jun 14, 2024 · Under the initiative, Brazil will develop its three-stage VLM rocket, which will be capable of deploying payloads of up to 150 kilograms to low Earth orbit at an altitude of 300 kilometres. The two-stage VS-50 sounding rocket …

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  11. Brazil Just Tested Its Largest Rocket Motor Ever, for …

    Oct 11, 2021 · Brazil successfully tested its largest rocket motor ever built, an innovative motor that will power a European rocket for scientific hypersonic experiments.

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  13. US20120234196A1 - Viscous Liquid Monopropellant

    This invention relates to the construction of a rocket motor and fuel system thereof and, in particular to a new and useful Viscous Liquid Monopropellant (VLM) rocket motor containing a...

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