SPACE TRANSPORTATION SYSTEM ON THE BASIS OF THE LIGHT, MIDDLE AND HEAVY CLASSES ROCKETS FAMILY WITH THE SPACE ROCKETS AERIAL LAUNCH FROM THE SURFACE-EFFECT AIRBORNE SHIP BOARD AND ITS FUNCTIONING METHOD Russian patent published in 2018 - IPC B64G1/00 

Abstract RU 2659609 C2

FIELD: astronautics.

SUBSTANCE: group of inventions relates to the field of aerospace equipment, namely to the space transportation system. In the space transportation system, for the different in weight cargo placement into the different by height and inclinations orbits space rockets (ILV) of light, medium and heavy classes on environmentally safe fuel components are used with the ILV aerial launch from the heavy surface-effect airborne ships boards. Carrier surface-effect airborne ship, moving near the surface-effect on the dynamic air cushion, delivers the loaded ILV to pre-selected areas over the World Ocean water area. Before the ILV airlift delivery, the carrier surface-effect airborne ship is taken away from the surface-effect, elevated to the required height, and performing the “zoom” maneuver. After the ILV airlift delivery and its removal to a safe distance from the carrier surface-effect airborne ship, performing the space rocket controlled turn into the optimal position, followed by the ILV first stage main engines staring-up.

EFFECT: improvement in the system energy and operational characteristics.

5 cl, 2 dwg

Similar patents RU2659609C2

Title Year Author Number
UNIVERSAL SPACE TRANSPORT SYSTEM BASED ON FAMILY OF SPACE ROCKETS OF LIGHT, MEDIUM AND HEAVY CLASSES WITH CARRIER ROCKETS LAUNCHING OVER WATER AREA OF WORLD OCEAN 2018
  • Kovalevskij Mikhail Markovich
  • Kovalevskij Aleksandr Sergeevich
RU2729912C1
AIRCRAFT ROCKET LAUNCH SITE FORMED ON BASIS OF SPACE-MISSION VEHICLE ADAPTED FROM TOPOL-M ICBM AND CARRIER AIRCRAFT IL-76MF FOR INSERTION OF SMALL SPACECRAFTS INTO FINAL ORBITS BY INSERTING SMV FROM AIRCRAFT USING COMBINED TRANSPORT-LAUNCHING PLATFORM AND LIFTING-STABILIZING PARACHUTE 2016
  • Kovalevskij Mikhail Markovich
  • Mekhonoshin Yurij Gennadevich
  • Chizhukhin Vladimir Nikolaevich
  • Chizhukhin Sergej Vladimirovich
RU2636447C2
METHOD FOR CONVERSION OF COMBAT SOLID-PROPELLANT ROCKETS INTO SOLID-PROPELLANT SPACE ROCKET AND SPACE ROCKET 1998
  • Solomonov Ju.S.
  • Sukhadol'Skij A.P.
  • Zinchenko S.M.
  • Vasil'Ev Ju.S.
  • Pilipenko P.B.
  • Frantsuzov V.A.
  • Andrjushin V.I.
RU2142898C1
ELECTRICAL AIR START SYSTEM OF THE SPACE ROCKET 2017
  • Leshchenko Vasilij Vasilevich
RU2658236C1
SPACE MISSILE AIR-BREATHING LAUNCH SYSTEM 2015
  • Leshchenko Vasilij Vasilevich
RU2620173C2
AERO-SPACE SYSTEM 1999
  • Karpov A.S.
  • Rachuk V.S.
  • Ivanov R.K.
  • Monakhov Ju.V.
  • Kovalevskij M.M.
  • Borisov A.V.
RU2160215C1
METHOD FOR CONTROL OF AERO-SPACE SYSTEMS FOR INJECTION OF PAYLOAD 1999
  • Karpov A.S.
  • Rachuk V.S.
  • Ivanov R.K.
  • Monakhov Ju.V.
  • Kovalevskij M.M.
  • Borisov A.V.
RU2160214C1
SPACE MISSILE AIR-BREATHING LAUNCH SYSTEM WITH THE ELECTRIC START 2016
  • Leshchenko Vasilij Vasilevich
RU2620172C1
COMPLEX SYSTEM FOR LAUNCHING HEAVY AEROSPACE SHUTTLES INTO ORBIT, SUPER-HEAVY JET AMPHIBIOUS AIRPLANE FOR SAID SYSTEM (VERSIONS) AND METHOD OF LAUNCHING 2008
  • Kobzev Viktor Anatol'Evich
  • Fortinov Leonid Grigor'Evich
  • Glombinskij Evgenij Nikolaevich
RU2397922C2
AEROSTATIC ROCKET AND SPACE COMPLEX 2017
  • Kozlov Aleksandr Ivanovich
  • Sorokin Sergej Aleksandrovich
  • Sasko Tatyana Prokofevna
  • Gulyaev Aleksandr Yurevich
RU2682893C1

RU 2 659 609 C2

Authors

Kovalevskij Mikhail Markovich

Teselkin Sergej Fedorovich

Tokhunts Arvid Drastomatovich

Dates

2018-07-03Published

2014-07-10Filed