FIELD: aerostation vehicles. SUBSTANCE: airship has envelopes 1 interconnected by means of wing 2, vertical and horizontal tails, pod 4 and engines 5. Airship is provided with vacuum pump connected with inner chamber of envelopes 1. Engines 5 are mounted on pylons 6 secured on envelopes 1. Vertical and horizontal tails are mounted in nose portion of pod 4. Horizontal tail is all-moving and vacuum; engines 5 are mounted in evacuated chambers; envelopes 1 are rigid and are provided with pneumatic valves 2. EFFECT: enhanced maneuverability and reduced noise of airship. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF FLIGHT AND AIRCRAFT TO THIS END | 2009 |
|
RU2410284C1 |
| POWER UNIT OF AEROSTATIC MODULE OF TRANSPORT SYSTEM | 2021 |
|
RU2796433C2 |
| HYBRID AIRCRAFT | 2008 |
|
RU2385257C1 |
| HIGHLY MANEUVERABLE AIRCRAFT | 1993 |
|
RU2070144C1 |
| SUPERSONIC MANEUVERABLE AIRCRAFT | 2000 |
|
RU2180309C2 |
| AERO-ENERGYSTAT | 2019 |
|
RU2703863C1 |
| MULTI-PURPOSE CRYOGENIC CONVERTIPLANE | 2009 |
|
RU2394723C1 |
| SEMI-RIGID AEROSTATIC FLYING VEHICLE WITH VARIABLE-CONFIGURATION CASE | 1994 |
|
RU2070136C1 |
| SUPERSONIC CONVERTIPLANE WITH X-SHAPED WING | 2015 |
|
RU2621762C1 |
| RECOVERABLE BOOSTER OF FIRST STAGE OF LAUNCH VEHICLE | 1999 |
|
RU2148536C1 |
