AEROSPACE CRAFT WITH NUCLEAR PROPULSOR AND AEROSPACE FLIGHTS PERFORMED THEREBY Russian patent published in 2016 - IPC B64D27/22 B64G1/40 B64C39/12 F25J3/04 

Abstract RU 2574295 C2

FIELD: aircraft engineering.

SUBSTANCE: claimed set can be used for atmosphere and space flights, at takeoff and retrieval. Aerospace craft features the canard-tail-less configuration. Nose airfoils and wings compose with the fuselage the delta-like airfoil. Nuclear rocket propeller comprises the heat exchange chamber coupled with the nuclear reactor via the radiation shielding. Atmosphere liquefied by the onboard liquefaction plants is used (partially) as the working fluid. Feeding and cooling onboard turboplants, turboelectric generators and the control jet engines are connected to the heat exchange chamber to operated directly at the cruising working fluid. With cruising nozzle cutoff the claimed nuclear propulsor incorporates the special-design shutoff device. In long-term aerospace flights the craft can be periodically refuelled with liquefied atmospheric medium.

EFFECT: higher efficiency, stability and controllability.

5 cl, 10 dwg

Similar patents RU2574295C2

Title Year Author Number
NUCLEAR ROCKET ENGINE 2012
  • Beljaev Vjacheslav Ivanovich
RU2521423C1
AEROSPACE AIRCRAFT (VERSIONS) 2008
  • Beljaev Vjacheslav Ivanovich
RU2397924C2
LIQUIDISING PLANT FOR AIRCRAFT 2012
  • Beljaev Vjacheslav Ivanovich
RU2521124C1
NUCLEAR ROCKET ENGINE 2008
  • Beljaev Vjacheslav Ivanovich
RU2370669C1
NUCLEAR REACTOR 2012
  • Beljaev Vjacheslav Ivanovich
RU2510652C1
AEROSPACE AIRCRAFT 2010
  • Kiselev Vladimir Vladimirovich
RU2436715C2
MULTIPLE-USE NUCLEAR ROCKET ENGINE 2020
  • Pisarev Aleksandr Nikolaevich
  • Senyavin Aleksandr Borisovich
  • Pavshuk Vladimir Aleksandrovich
RU2760079C1
NUCLEAR REACTOR 2019
  • Belyaev Vyacheslav Ivanovich
RU2757160C2
AQUA AEROSPACE VEHICLE 2012
  • Kiselev Vladimir Vladimirovich
  • Vagulin Vladimir Viktorovich
RU2626418C2
METHOD AND AIR VEHICLE FOR MOVING IN PLANETARY ATMOSPHERE WITH SPEEDS ABOVE THE FIRST SPACE AND HIGHLY INTEGRATED HYPERSONIC VEHICLE APPARATUS (VERSIONS) FOR IMPLEMENTATION OF THE METHOD 2012
  • Aleksandrov Oleg Aleksandrovich
RU2618831C2

RU 2 574 295 C2

Authors

Beljaev Vjacheslav Ivanovich

Dates

2016-02-10Published

2013-12-16Filed