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SU1811129A1 - Method of flying of hypersonic, suborbital and space vehicles - Google Patents

Method of flying of hypersonic, suborbital and space vehicles

Info

Publication number
SU1811129A1
SU1811129A1 SU2279112/23A SU2279112A SU1811129A1 SU 1811129 A1 SU1811129 A1 SU 1811129A1 SU 2279112/23 A SU2279112/23 A SU 2279112/23A SU 2279112 A SU2279112 A SU 2279112A SU 1811129 A1 SU1811129 A1 SU 1811129A1
Authority
SU
USSR - Soviet Union
Prior art keywords
flying
suborbital
hypersonic
attack
space vehicles
Prior art date
Application number
SU2279112/23A
Other languages
Russian (ru)
Inventor
И.И. Шунейко
Original Assignee
И.И. Шунейко
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by И.И. Шунейко filed Critical И.И. Шунейко
Priority to SU2279112/23A priority Critical patent/SU1811129A1/en
Application granted granted Critical
Publication of SU1811129A1 publication Critical patent/SU1811129A1/en

Links

Classifications

    • 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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242—Orbits and trajectories

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Navigation (AREA)

Abstract

FIELD: handling of flying vehicles. SUBSTANCE: active ricochet is performed in quasihorizontal flight. To this end, flying vehicle is turned to optimal angle of attack after ballistic phase at descent altitude and thrust pulse is created along longitudinal axis by turning speed vector and compensating for speed losses. The flying vehicle is brought to next ballistic phase at angle of attack corresponding to maximum aerodynamic efficiency. EFFECT: increased flying range. 1 dwg
SU2279112/23A 1976-09-03 1976-09-03 Method of flying of hypersonic, suborbital and space vehicles SU1811129A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2279112/23A SU1811129A1 (en) 1976-09-03 1976-09-03 Method of flying of hypersonic, suborbital and space vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2279112/23A SU1811129A1 (en) 1976-09-03 1976-09-03 Method of flying of hypersonic, suborbital and space vehicles

Publications (1)

Publication Number Publication Date
SU1811129A1 true SU1811129A1 (en) 1996-10-10

Family

ID=60538412

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2279112/23A SU1811129A1 (en) 1976-09-03 1976-09-03 Method of flying of hypersonic, suborbital and space vehicles

Country Status (1)

Country Link
SU (1) SU1811129A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2520629C1 (en) * 2012-11-19 2014-06-27 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Method to control spacecraft placing into orbit of planet artificial satellite
RU2531679C2 (en) * 2012-08-21 2014-10-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Омский государственный технический университет" Method of clearing space debri from orbit
RU2575556C2 (en) * 2014-02-14 2016-02-20 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Control over spacecraft at orbiting of artificial satellite orbit
RU2583507C1 (en) * 2015-02-05 2016-05-10 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Method for simultaneously putting group of satellites into non-coplanar orbits (versions)
RU2666011C1 (en) * 2017-07-21 2018-09-05 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Method of fast delivery of the useful load

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2531679C2 (en) * 2012-08-21 2014-10-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Омский государственный технический университет" Method of clearing space debri from orbit
RU2520629C1 (en) * 2012-11-19 2014-06-27 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Method to control spacecraft placing into orbit of planet artificial satellite
RU2575556C2 (en) * 2014-02-14 2016-02-20 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Control over spacecraft at orbiting of artificial satellite orbit
RU2583507C1 (en) * 2015-02-05 2016-05-10 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Method for simultaneously putting group of satellites into non-coplanar orbits (versions)
RU2666011C1 (en) * 2017-07-21 2018-09-05 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Method of fast delivery of the useful load

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