SU1826442A1 - Hypersonic space complex - Google Patents
Hypersonic space complexInfo
- Publication number
- SU1826442A1 SU1826442A1 SU2279113/23A SU2279113A SU1826442A1 SU 1826442 A1 SU1826442 A1 SU 1826442A1 SU 2279113/23 A SU2279113/23 A SU 2279113/23A SU 2279113 A SU2279113 A SU 2279113A SU 1826442 A1 SU1826442 A1 SU 1826442A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- complex
- hypersonic
- flying vehicle
- propellant
- engines
- Prior art date
Links
- 239000003380 propellant Substances 0.000 abstract 3
- 239000004215 Carbon black (E152) Substances 0.000 abstract 1
- 229930195733 hydrocarbon Natural products 0.000 abstract 1
- 150000002430 hydrocarbons Chemical class 0.000 abstract 1
- 229910052739 hydrogen Inorganic materials 0.000 abstract 1
- 239000001257 hydrogen Substances 0.000 abstract 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 abstract 1
- 238000002347 injection Methods 0.000 abstract 1
- 239000007924 injection Substances 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/14—Space shuttles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/401—Liquid propellant rocket engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
Abstract
FIELD: hypersonic space flying vehicles. SUBSTANCE: complex has airframe of hypersonic flying vehicle of aeroplane configuration with delta wing 9 triangular in plan and vertical tail 10, fuselage of flying vehicle which is aerodynamically integrated with wing has cargo compartment and tail section 6; complex is provided with cruise jet engines 8 which can operate on hydrogen propellant and hydrocarbon propellant; complex has V-shaped recess for mounting either booster (bipropellant tank 13 and additional liquid-propellant rocket engines 14 in version of injection of useful loads into space or two or more tanks of lesser capacity (without additional engines) in version of hypersonic aeroplane (airliner). Standard flight modes of flying vehicle: motion in atmosphere at ascent and descent at maximum aerodynamic efficiency over wavy trajectory (at suborbital speed in upper atmosphere at altitudes of 70 to 100 km). EFFECT: extended field of application and enhanced aerodynamic efficiency of complex. 6 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2279113/23A SU1826442A1 (en) | 1976-09-03 | 1976-09-03 | Hypersonic space complex |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2279113/23A SU1826442A1 (en) | 1976-09-03 | 1976-09-03 | Hypersonic space complex |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1826442A1 true SU1826442A1 (en) | 1995-05-10 |
Family
ID=60537321
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2279113/23A SU1826442A1 (en) | 1976-09-03 | 1976-09-03 | Hypersonic space complex |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1826442A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2568630C1 (en) * | 2014-06-26 | 2015-11-20 | Николай Евгеньевич Староверов | Space rocket and method of its landing (versions) |
RU2596004C2 (en) * | 2015-01-20 | 2016-08-27 | Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) | Method for controlling spacecraft motion on active section of placing it into the orbit of planet artificial satellite |
RU2758725C1 (en) * | 2021-03-03 | 2021-11-01 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" | Aircraft for intercontinental flights in the stratosphere |
-
1976
- 1976-09-03 SU SU2279113/23A patent/SU1826442A1/en active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2568630C1 (en) * | 2014-06-26 | 2015-11-20 | Николай Евгеньевич Староверов | Space rocket and method of its landing (versions) |
RU2596004C2 (en) * | 2015-01-20 | 2016-08-27 | Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) | Method for controlling spacecraft motion on active section of placing it into the orbit of planet artificial satellite |
RU2758725C1 (en) * | 2021-03-03 | 2021-11-01 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" | Aircraft for intercontinental flights in the stratosphere |
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