Normally open pyrovalve before activation. The fluid can still pass.
Normally open pyrovalve after activation. The piston has cut off the flow.
Normally closed pyrovalve before activation. The fluid is blocked.
Normally closed pyrovalve after activation. The fluid can now flow.
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References
- ↑ "Pyrotechnic Valves for Space Propulsion Systems". space-propulsion.com. Retrieved 29 August 2022.
- ↑ "Pyrovalve". eaton.com. Retrieved 29 August 2022.
- ↑ R. Lescouzères, M. Wolf, B. Wollenhaupt, S. Goodburn, M. Peukert, T. Biehler, M. Abele, M. Pastorino, T. Walloschek. "Propulsion System Development and Verification Activities for the 2016 ExoMars Trace Gas Orbiter" (PDF). pp. 2–3. Retrieved 29 August 2022.
{{cite web}}: CS1 maint: multiple names: authors list (link) - ↑ "Cobham Mission Systems' Pyrovalves power precision NASA Perseverance Rover Mars landing" . Retrieved 29 August 2022.