FIELD: astronautics.
SUBSTANCE: group of inventions relates to space engineering. In the method, the system for providing access to the outer space contains a space carrier vehicle with one or more rocket engines. Said space carrier vehicle is configured to execute activities including launching of at least one of said one or more rocket engines for launching said space carrier vehicle with its nose part being positioned forward; positioning the space carrier vehicle with its tail part looking forward to re-enter the atmosphere of the Earth; landing the space carrier vehicle on a landing structure on the water surface with its tail part looking forward by using thrust from at least one or more of the specified rocket engines. In the second version, the system to provide access to the outer space contains a space carrier vehicle, wherein the space carrier vehicle includes one or more ignitable rocket engines made with the ability to launch the space carrier vehicle with its nose part looking forward, one or more thrusters configured to position the space carrier vehicle in such a way that its tail part is looking forward to re-enter the atmosphere, a control surface made with the ability to turn after the launch of the space carrier vehicle and before the space carrier vehicle touches the landing structure on water in such a way its tail part is looking forward by using thrust from at least one or more of above rocket engines.
EFFECT: technical result of the group of inventions is to increase the efficiency of the system.
37 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
CARRIER ROCKET SEA SURFACING AND APPROPRIATE SYSTEMS AND METHODS | 2010 |
|
RU2558166C2 |
DEVICE FOR LANDING OF RETURN STAGE OF CARRIER ROCKET | 2020 |
|
RU2740525C1 |
MULTI-ELEMENT COMPOSITE AEROSPACE COMPLEX FOR VERTICAL TAKE-OFF AND LANDING IN THE SEA LAUNCH SYSTEM | 2021 |
|
RU2769791C1 |
METHOD OF USING THE REUSABLE FIRST STAGE OF A LAUNCH VEHICLE | 2017 |
|
RU2678616C1 |
METHOD OF LAUNCHING PAYLOAD INTO ORBIT AND REUSABLE CR EJECTOR STAGE FOR ITS IMPLEMENTATION | 2019 |
|
RU2734965C1 |
METHOD FOR OPERATION OF LAUNCH VEHICLES AND SET OF ROCKET BOOSTERS FOR ITS REALIZATION | 2002 |
|
RU2242407C2 |
CARRIER ROCKET | 2011 |
|
RU2482030C2 |
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 |
|
RU2729912C1 |
RECOVERABLE BOOSTER OF FIRST STAGE OF LAUNCH VEHICLE | 1999 |
|
RU2148536C1 |
REUSABLE MISSILE AND AIRCRAFT UNIT AND WAY TO RETURN IT TO SPACEPORT | 2010 |
|
RU2442727C1 |
Authors
Dates
2019-03-26—Published
2010-06-14—Filed