DLVD – Dual Flow Bibpropellant Latching Valve Development

The project aims at preparation (to TLR 4) of the dual flow, latching control valve for the satellite apogee engines. This includes development and tests of the valve actuator (Astornika) followed by the development and tests of the complete valve assembly (ŁRN-IoA). The valve is foreseen to be used with standard (MMH, MON) as well as green (HTP) propellants.

Project coordinator: dr inż. Dominik Kublik
Phone: (+ 48) 22 846 00 11 ext. 531
E-mail: dominik.kublik@ilot.lukasiewicz.gov.pl
Project duration: 01.04.2020 – 01.04.2022
Funding institution: European Space Agency
Programme name: ESA – PLIIS
Consortium: Łukasiewicz Research Network – Institute of Aviation, Astronika

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