{"id":4102,"date":"2022-02-11T14:58:00","date_gmt":"2022-02-11T13:58:00","guid":{"rendered":"https:\/\/www.nlr.org\/?p=4102"},"modified":"2024-12-13T11:40:21","modified_gmt":"2024-12-13T10:40:21","slug":"ontwikkeling-van-een-mini-parallel-micropomp","status":"publish","type":"post","link":"https:\/\/www.nlr.org\/nl\/newsroom\/case\/ontwikkeling-van-een-mini-parallel-micropomp\/","title":{"rendered":"Ontwikkeling van een mini parallel micropomp"},"content":{"rendered":"\n

Ontwikkeling van een mini parallel micropomp<\/strong><\/p>\n\n\n\n

De uitdaging<\/h2>\n\n\n\n

De kosten voor ontwikkeling, productie en lancering van CubeSats zijn erg laag, in vergelijking met conventionele satellieten. Dit heeft geleid tot interesse van de industrie om eigen CubeSats te ontwikkelen. Het streven van de industrie naar volume- en massa-optimalisatie heeft geleid tot miniaturisering van elektronica in CubeSats. Om de kosten laag te houden, wordt er gebruik gemaakt van kant-en-klare, commercieel verkrijgbare elektronica die zeer kosteneffectief is, maar een klein operationeel temperatuurbereik heeft. De relatief hoge vermogensdichtheid van CubeSats betekent dat er in hetzelfde volume meer vermogen wordt omgezet in warmte, waardoor de componenten sneller opwarmen. De thermische problemen worden verergerd door de introductie van voortstuwingsmodules voor CubeSats, die zelf ook een grote hoeveelheid warmte produceren. Zonder voldoende warmteafvoer kunnen de componenten van de CubeSat snel oververhit raken.<\/p>\n\n\n\n

\n

De oplossing<\/h2>\n\n\n\n

Conventionele methoden om deze warmte af te voeren, zoals heatpipes, zijn niet langer geschikt. Mechanisch gepompte lussen vormen een haalbare oplossing om deze warmte af te voeren, omdat ze effici\u00ebnter zijn. Deze lussen zijn echter doorgaans duur en vereisen veel kleinere massastromen in vergelijking met grotere satellieten. Om een kleinere mechanisch gepompte lus te cre\u00ebren, is een kleinere, flexibele pomp nodig. Dat is het doel van de MPMP (Multi Parallel Micro Pump). Een consortium van Demcon Kryoz, ISISpace en Koninklijke NLR wil met steun van de Europese Ruimtevaartorganisatie (ESA) een MPMP ontwikkelen voor gebruik in kleine satellieten.<\/p>\n\n\n\n

\"Thermal<\/figure>\n<\/div>\n\n\n\n

Wat doen wij?<\/h2>\n\n\n\n
\n
\n

De Multi Parallel Micro Pump (MPMP) bestaat uit een opeenstapeling (stack) van meerdere micropompen, elk bestaand uit een pi\u00ebzo-membraan en een klep om de stroming te sturen. De belangrijkste functionaliteit schuilt in de flexibiliteit die de huidige oplossing biedt: als er een grotere capaciteit nodig is, kunnen er meer pompen worden toegevoegd om dat te kunnen leveren. Dit komt ook de robuustheid ten goede. Voor typische ruimtevaarttoepassingen worden dure pompen gebruikt en vanwege redundantie wordt er ook nog een tweede back-up toegevoegd. Als er bijvoorbeeld 20 micropompen in \u00e9\u00e9n stack geplaatst zijn,<\/p>\n<\/div>\n\n\n\n

<\/div>\n\n\n\n
\n

zal het verlies van \u00e9\u00e9n enkele pomp niet leiden tot verlies van functionaliteit van de lus, maar zal de flow met 5% verlagen. Momenteel hebben we een prototype van een MPMP op ware grootte, waarmee een massastroom van 500 mg\/s is aangetoond, voldoende om minimaal 20 watt aan warmte te transporteren. Het consortium wil het ontwerp zodanig verbeteren dat er minimaal 100 watt aan warmte van een warmtebron, zoals een CubeSat-voortstuwingsmodule, naar een koellichaam elders in de satelliet kan worden getransporteerd.<\/p>\n<\/div>\n<\/div>\n\n\n\n

\n
\n
\n
\n

Project partners:<\/strong>
Industrie (EU): Demcon Kryoz, ISISpace
Onderzoeksorganisaties: Koninklijke NLR, ESA
Start : 2021
Tijdsduur: 2 jaar<\/em><\/p>\n<\/div>\n\n\n\n

<\/div>\n<\/div>\n<\/div>\n<\/div>\n","protected":false},"excerpt":{"rendered":"

Ontwikkeling van een mini parallel micropomp De uitdaging De kosten voor ontwikkeling, productie en lancering van CubeSats zijn erg laag, in vergelijking met conventionele satellieten. Dit heeft geleid tot interesse van de industrie om eigen CubeSats te ontwikkelen. Het streven van de industrie naar volume- en massa-optimalisatie heeft geleid tot miniaturisering van elektronica in CubeSats. 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