UA56457U - Method of launching rocket of "packet" scheme from launching structure of ground facility - Google Patents
Method of launching rocket of "packet" scheme from launching structure of ground facilityInfo
- Publication number
- UA56457U UA56457U UAU201010333U UAU201010333U UA56457U UA 56457 U UA56457 U UA 56457U UA U201010333 U UAU201010333 U UA U201010333U UA U201010333 U UAU201010333 U UA U201010333U UA 56457 U UA56457 U UA 56457U
- Authority
- UA
- Ukraine
- Prior art keywords
- launching
- rocket
- collector
- compressed gas
- supplied
- Prior art date
Links
Landscapes
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
A method of launching a rocket of "packet" scheme from a launching structure of ground facility comprises installation of the rocket on the launcher, supply of compressed gas in the rocket engine area for 15 seconds prior to launching through a pipe with a controllable valve and a ring collector of launching facility with nozzles-sprinklers. In the ring collector the pressure is maintained for more than 0.6 MPa and at the same time compressed gas is supplied into the area of rocket engines through the nozzles-sprinklers of an additional collector of launcher by connecting additional collector with two additional co-controlled pipes. When the pressure drops to 0.6 MPa compressed gas is supplied in two auxiliary lines in the ring collector and at the same time the compressed gas is supplied in three redundant control lines together in the additional collector. During repeated pressure drops to 0.6 MPa compressed gas is supplied in two emergency lines into the ring collector.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAU201010333U UA56457U (en) | 2010-08-25 | 2010-08-25 | Method of launching rocket of "packet" scheme from launching structure of ground facility |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAU201010333U UA56457U (en) | 2010-08-25 | 2010-08-25 | Method of launching rocket of "packet" scheme from launching structure of ground facility |
Publications (1)
Publication Number | Publication Date |
---|---|
UA56457U true UA56457U (en) | 2011-01-10 |
Family
ID=50829753
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAU201010333U UA56457U (en) | 2010-08-25 | 2010-08-25 | Method of launching rocket of "packet" scheme from launching structure of ground facility |
Country Status (1)
Country | Link |
---|---|
UA (1) | UA56457U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2733449C1 (en) * | 2020-02-12 | 2020-10-01 | Николай Федорович Шаповалов | Launching complex and method for launching carrier rockets without using the first stage |
-
2010
- 2010-08-25 UA UAU201010333U patent/UA56457U/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2733449C1 (en) * | 2020-02-12 | 2020-10-01 | Николай Федорович Шаповалов | Launching complex and method for launching carrier rockets without using the first stage |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2009011497A3 (en) | Fuel gas supply system and method of ship | |
WO2013126122A3 (en) | Bleed air and hot section component cooling air system of a gas turbine and method | |
EP2784270A3 (en) | Fuel and actuation system for gas turbine engine | |
EA033564B1 (en) | System and method for power generation | |
WO2010096817A3 (en) | Combustion system | |
EP2607655A3 (en) | Intake liner for a gas turbine engine | |
MY153186A (en) | Internal combustion engine, vehicle, marine vessel, and secondary air supply method for internal combustion engine | |
WO2011162988A3 (en) | High nitrogen and other inert gas anti-corrosion protection in wet pipe fire protection system | |
GB201201899D0 (en) | Onboard inert gas generation system | |
WO2015019011A3 (en) | Device for supplying rocket engine propellant | |
GB201312087D0 (en) | Fuel circuit of an aeronautical turbine engine having a fuel pressure regulating valve | |
EP2500552A3 (en) | Dual pump fuel flow system for a gas turbine engine and method of controlling | |
WO2019194670A8 (en) | Gas treatment system and ship including same | |
WO2014014536A3 (en) | Systems and methods for preventing fuel leakage in a gas turbine engine | |
CN103711610A (en) | RBCC fuel gas generator integrated supplying and adjusting system based on liquid oxygen | |
WO2012007638A3 (en) | A solution for controlling a turbo compressor | |
UA56457U (en) | Method of launching rocket of "packet" scheme from launching structure of ground facility | |
EP3617456A3 (en) | Oil supply assembly for gas turbine engine | |
AU2012358130B2 (en) | Method and device for controlling the fuel supply of an internal combustion engine operated with liquefied gas | |
WO2012084347A3 (en) | Gas turbine and method for oparating said gas turbine | |
EP2343444A3 (en) | Fuel control arrangements for a gas turbine engine | |
WO2012001391A3 (en) | Steam turbine and steam generator system and operation thereof | |
WO2013003544A3 (en) | Methods and systems for controlling fuel systems of internal combustion engines | |
KR20180084212A (en) | The fuel cell system removing the high-pressurized line in the hydrogen supplying system and control method thereof | |
UA103528C2 (en) | Method for control of traction vector of liquid-propellant rocket engine and liquid-propellant rocket engine for its realization |