RU93003557A - AIRCRAFT ENGINE - Google Patents

AIRCRAFT ENGINE

Info

Publication number
RU93003557A
RU93003557A RU93003557/23A RU93003557A RU93003557A RU 93003557 A RU93003557 A RU 93003557A RU 93003557/23 A RU93003557/23 A RU 93003557/23A RU 93003557 A RU93003557 A RU 93003557A RU 93003557 A RU93003557 A RU 93003557A
Authority
RU
Russia
Prior art keywords
aircraft
launch vehicle
engine
space
aircraft engine
Prior art date
Application number
RU93003557/23A
Other languages
Russian (ru)
Inventor
Л.И. Кириллов
Original Assignee
Л.И. Кириллов
Filing date
Publication date
Application filed by Л.И. Кириллов filed Critical Л.И. Кириллов
Publication of RU93003557A publication Critical patent/RU93003557A/en

Links

Claims (1)

Авиакосмический двигатель содержит диффузор, камеру сгорания, сопло, магнитоэлектрический переключатель, соединенный стержнем с золотником, конус и тормозные устройства, позволяющие создавать стартовую тягу, взлетать как самолет и работать как ПВРД, подниматься на космическую орбиту вокруг Земли, при возвращении использовать энергию нагрева в верхних слоях атмосферы для торможения скорости спускающегося летательного аппарата и совершать посадку, как обычный самолет. В отличие от ракетоносителя не оставляет в космосе отработанные ступени ракетоносителя, экономно расходует кислород за счет атмосферного воздуха. Авиакосмический двигатель предназначен для летательных аппаратов типа "Буран" и переоборудованного самолета "ТУ-160" и на его основе можно создать авиационный двигатель.The aerospace engine contains a diffuser, a combustion chamber, a nozzle, a magnetoelectric switch connected by a rod with a valve, a cone and braking devices that allow you to create a starting thrust, take off like an airplane and work like a ramjet, go up into space orbit around the Earth, returning to use heating energy in the upper layers of the atmosphere to slow down the speed of the descending aircraft and land like an ordinary plane. Unlike the launch vehicle, it does not leave the spent launch vehicle stages in space; it economically consumes oxygen due to atmospheric air. The aerospace engine is designed for Buran-type aircraft and the converted TU-160 aircraft, and an aircraft engine can be created on its basis.
RU93003557/23A 1993-01-22 AIRCRAFT ENGINE RU93003557A (en)

Publications (1)

Publication Number Publication Date
RU93003557A true RU93003557A (en) 1995-08-27

Family

ID=

Similar Documents

Publication Publication Date Title
RU93043825A (en) COMBINED AIRCRAFT
CN206206009U (en) A kind of rocket ramjet
RU93003557A (en) AIRCRAFT ENGINE
GB1151413A (en) Improvements in Jet-Propelled Aeroplanes
GB1066268A (en) Jet propulsion power plant
FR2349495A1 (en) Vtol aircraft with circular wing - forces air radially outwards over ring of aerofoil section
GB572876A (en) Improvements in or relating to fluid reaction apparatus for propelling purposes
GB1010100A (en) Improvements in or relating to vtol or stol aircraft
CUMMINGS Experience with low cost jet engines(Design and fabrication of low cost turbojet and turbofan engines)
GB857037A (en) Improved power unit
CONWAY The development of an integrated propulsion system for jet STOL flight research(performance tests of augmentor-wing powered lift concept)
BOURGEOIS et al. Some aerodynamic problems related to the propulsion of a hypersonic airplane(Effects of air intake and exhaust nozzle properties on hypersonic ramjet power plant)
RU2041392C1 (en) Gas-phase nuclear rocket engine with thrust augmentation
WILSON, III et al. CTOL, STOVL, and VTOL fighter design comparisons
Hewitt Air breathing propulsion for advanced orbital launch vehicles
TREFNY et al. Overview of NASP nozzle research
GB898358A (en) Vertical take-off aircraft
RU1821408C (en) Toroidal airship
Lardellier et al. Air breathing combined engines for space transportation systems
Kumakawa et al. A study of reusable launcher/demonstrator powered by aerospike engines
GB998774A (en) V/stol aircraft with propelling, lifting and orientable jet nozzles
FRANCISCUS Jet noise of an augmentor wing-advanced supersonic transport(Analysis of jet noise produced by supersonic transport aircraft with augmentor wing and four duct burning turbofan engines)
Chevis Advanced developments in turbo machinery for use in small RPV engines
LEWIS Future military powerplants((fighter aircraft engines))
RU93030224A (en) AEROSPACE TRANSPORT SYSTEM