Downwash vectoring louvers are the mechanism the source dossier attributes to the Focke Rochen for achieving forward flight from a vertical-lift configuration. The source states that "the Fw-Rochen would have achieved forward flight by vectoring the downwash from the propellers rearward through a series of louvers below them."
Claimed operation
- The Contra-Rotating Propellers in the Circular-Wing Annular-Duct Configuration produce a downward flow for vertical lift.
- A series of louvers below the propellers redirects that flow rearward, producing forward thrust.
- "The louvers themselves could also be completely closed for gliding flight in the event of engine failure" — that is, the closed position is claimed to restore a gliding configuration.
Evidence status
The source describes the mechanism entirely in the conditional mood ("would have achieved"). The Rochen was never built, and the page reports no wind-tunnel or flight data for the louver arrangement. The claim is therefore recorded as a design proposal, not a demonstrated result.
Related mechanisms on the same aircraft
- Auxiliary Combustion Chambers (Rochen) — the trailing-edge afterburner arrangement claimed to provide horizontal flight.
- VTOL Aircraft — the operational category.
Source notes & attribution
- Rex Research, "Heinrich FOCKE: Helicopter Glider," https://rexresearch.com/FockeRochen/FockeRochen.html (retrieved 2026-09-17).
- https://rexresearch.com/FockeRochen/FockeRochen.html