UA98727U - Air space complex - Google Patents

Air space complex

Info

Publication number
UA98727U
UA98727U UAU201410949U UAU201410949U UA98727U UA 98727 U UA98727 U UA 98727U UA U201410949 U UAU201410949 U UA U201410949U UA U201410949 U UAU201410949 U UA U201410949U UA 98727 U UA98727 U UA 98727U
Authority
UA
Ukraine
Prior art keywords
fuselage
rocket
cargo compartment
longitudinal element
carrier aircraft
Prior art date
Application number
UAU201410949U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Volodymyr Petrovych Kharchenko
Yurii Ivanovych Sviashchenko
Volodymyr Mykolaiovych Dikhtiarenko
Viacheslav Pavlovych Korcheniuk
Oleksandr Opanasovych Udovenko
Original Assignee
Univ Nat Aviation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Univ Nat Aviation filed Critical Univ Nat Aviation
Priority to UAU201410949U priority Critical patent/UA98727U/en
Publication of UA98727U publication Critical patent/UA98727U/en

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Abstract

Авіаційний космічний комплекс включає в себе літак-носій з верхніми та нижніми цільноповоротними крилами з від'ємною стрілоподібністю, двигунами, фюзеляжем з вирізом по борту і вантажним відсіком по борту, ракету-носій, що розміщена у вантажному відсіку фюзеляжу і виступає за контур фюзеляжу, і прикрита термокришкою, що скріплена замками з краями вирізу і з ракетою-носієм фіксаторами, повздовжній елемент під термокришкою вздовж борту, який виконано поворотним по горизонталі і зв'язаний по своїх кінцях з бортом літака-носія і з задньою частиною ракети-носія шарнірними вузлами, що відділяються. Вказаний повздовжній елемент виконано з двох телескопічних розсувних деталей.The aerospace complex includes a carrier aircraft with upper and lower integral wings with a negative sweep, engines, fuselage with a cutout on the side and cargo compartment on the board, a launch vehicle placed in the cargo compartment of the fuselage and the fuselage protrusion and covered by a thermal cover fastened with locks with cutout edges and with a launch rocket, a longitudinal element under the thermal cover along the side, which is rotatable horizontally and connected at its ends to the side of the carrier aircraft and to the rear. by the sloping rocket of detachable hinged knots. The specified longitudinal element is made of two telescopic sliding parts.

UAU201410949U 2014-10-07 2014-10-07 Air space complex UA98727U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201410949U UA98727U (en) 2014-10-07 2014-10-07 Air space complex

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201410949U UA98727U (en) 2014-10-07 2014-10-07 Air space complex

Publications (1)

Publication Number Publication Date
UA98727U true UA98727U (en) 2015-05-12

Family

ID=53674591

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201410949U UA98727U (en) 2014-10-07 2014-10-07 Air space complex

Country Status (1)

Country Link
UA (1) UA98727U (en)

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