Device for reducing aerodynamic drag of a vehicale
A device for reducing the aerodynamic drag of a vehicle includes at least one masking element for at least one part of a nozzle of the vehicle's engine, the masking element having a resorbable material designed to be eliminated in the nozzle's flow once the engine is ignited. A space craft includes the nozzle attached to the fuselage of the space craft.
1. A device for reducing the aerodynamic drag of a vehicle, equipped with at least one engine fitted with a jet pipe propelling nozzle projecting beyond the rear of the vehicle's fuselage and getting wider the farther away it extends from the rear of the vehicle's fuselage, the device comprising at least one masking element for at least one part of the nozzle, the masking element comprising resorbable material designed to be eliminated in the nozzle's flow once the engine is ignited wherein said masking element is a cover prolonging the vehicle's fuselage externally beyond the nozzle and aerodynamically shaped to reduce the aerodynamic drag of the vehicle.
2. The device according to claim 1 wherein said cover is shaped in a generally conical shape, the diameter of the cover decreasing as the cover extends farther away from the fuselage.
3. The device according to claim 2 wherein the cover comprises a distal opening opposite the nozzle opening.
4. The device according to claim 3 wherein the distal opening has a smaller diameter with respect to the nozzle's opening.
5. The device according to claim 3 wherein the distal opening is part of a channel of reduced diameter and is coaxial with the axis of the cover, the channel designed to let the engine be ventilated during a part of the vehicle's flight with the engine not yet ignited and to allow the engine's jet to establish itself.
6. The device according to claim 1 wherein the resorbable material is a foam material.
7. The device according to claim 6 wherein the foam material is one of expanded polystyrene, melamine foam, expanded PVC, and polyurethane foam.
8. The device according to claim 1 wherein the resorbable material is covered by a skin for a better surface condition.
9. The device according to claim 1 wherein the resorbable material is a fire-proofed material.
10. A space craft comprising a device according to claim 1 wherein the device is attached to the fuselage.
11. The space craft according to claim 10 wherein the fuselage extends around a combustion chamber of the engine.
12. The space craft according to claim 10 wherein the fuselage extends around at least one part of the nozzle of said engine.
13. The space craft according to claim 10 wherein the masking element is secured to the rear of the fuselage of the vehicle by a removable fixing means.
14. The space craft according to claim 13 wherein the removable fixing means comprises a ring element.
15. The space craft according to claim 13 wherein the removable fixing means is designed to be detachable, the removable fixing means remaining fixed on the vehicle's fuselage after combustion of the masking element.
16. A device for reducing the aerodynamic drag of a vehicle, equipped with at least one engine fitted with a jet pipe propelling nozzle projecting beyond the rear of the vehicle's fuselage and getting wider the farther away it extends from the rear of the vehicle's fuselage, the device comprising at least one masking element for at least one part of the nozzle, the masking element comprising resorbable material designed to be eliminated in the nozzle's flow once the engine is ignited, wherein said masking element is a cover in a generally conical shape prolonging the vehicle's fuselage externally beyond the nozzle, the diameter of the cover decreasing as the cover extends farther away it gets from the fuselage.
17. The device according to claim 16 wherein the cover comprises a distal opening opposite the nozzle opening.
18. The device according to claim 17 wherein the distal opening has a smaller diameter with respect to the nozzle's opening.
19. The device according to claim 17 wherein the distal opening is part of a channel of reduced diameter and is coaxial with the axis of the cover, the channel designed to let the engine be ventilated during a part of the vehicle's flight with the engine not yet ignited and to allow the engine's jet to establish itself.
20. The device according to claim 16 wherein the resorbable material is a foam material.
21. The device according to claim 20 wherein the foam material is one of expanded polystyrene, melamine foam, expanded PVC, and polyurethane foam.
22. The device according to claim 16 wherein the resorbable material is covered by a skin for a better surface condition.
23. The device according to claim 16 wherein the resorbable material is a fire-proofed material.
24. A space craft comprising a device according to claim 16 wherein the device is attached to the fuselage.
25. The space craft according to claim 24 wherein the fuselage extends around a combustion chamber of the engine.
26. The space craft according to claim 24 wherein the fuselage extends around at least one part of the nozzle of said engine.
27. The space craft according to claim 24 wherein the masking element is secured to the rear of the fuselage of the vehicle by a removable fixing means.
28. The space craft according to claim 27 wherein the removable fixing means comprises a ring element.
29. The space craft according to claim 27 wherein the removable fixing means is designed to be detachable, the removable fixing means remaining fixed on the vehicle's fuselage after combustion of the masking element.