FIELD: transport.
SUBSTANCE: proposed is the method of deployment and altitude suspension of data system comprising carrier aircraft (CA) with data acquisition, processing and transmission hardware and base servicing module connected therewith by steel rope system. Carrier aircraft is placed in stable wind flow of atmosphere tropo pause zone and kept therein by means of aircraft control surfaces and steel rope relative to earth surface. Placing aircraft to operating altitude is performed by midair towing exploiting aerodynamic properties of aircraft while descent and landing after completed flight program (or in the case of failures) is effected by controlled gliding after unlatching the towing rope. Carrier aircraft represents hydride airplane "glider - kite" that features "duck" aerodynamic profile with high aerodynamic characteristics and low specific load onto wing.
EFFECT: longer continuous flight and higher stability, reduced costs.
6 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
HYPERSONIC AIRCRAFT | 2009 |
|
RU2393978C1 |
MULTI-FUNCTIONAL FLYING VEHICLE | 2000 |
|
RU2169104C1 |
AERODYNAMIC INTEGRATED TELECOMMUNICATION SYSTEM | 2001 |
|
RU2180767C1 |
METHOD OF LOCATING HIGH-ALTITUDE PLATFORM AND HIGH-ALTITUDE PLATFORM | 2012 |
|
RU2506204C1 |
METHOD OF WIND AND ENERGY AIR FLOWS ENERGY CONVERSION AT MEDIUM ALTITUDES IN TROPOSPHERE AND DEVICE FOR ITS IMPLEMENTATION | 2019 |
|
RU2721014C1 |
TANKER AEROPLANE | 1994 |
|
RU2100257C1 |
METHOD FOR INTERORBIT TRANSPORTATION OF PAYLOADS | 2009 |
|
RU2404091C1 |
TANKER AEROPLANE | 1994 |
|
RU2142897C1 |
AERO-ENERGYSTAT | 2019 |
|
RU2703863C1 |
HIGH-CAPACITY AIRCRAFT | 2007 |
|
RU2335430C1 |
Authors
Dates
2010-06-20—Published
2009-01-13—Filed