RU94001670A - Method of injection of payload into orbit - Google Patents

Method of injection of payload into orbit

Info

Publication number
RU94001670A
RU94001670A RU94001670/11A RU94001670A RU94001670A RU 94001670 A RU94001670 A RU 94001670A RU 94001670/11 A RU94001670/11 A RU 94001670/11A RU 94001670 A RU94001670 A RU 94001670A RU 94001670 A RU94001670 A RU 94001670A
Authority
RU
Russia
Prior art keywords
payload
vehicle
launch vehicle
carrier
stage
Prior art date
Application number
RU94001670/11A
Other languages
Russian (ru)
Other versions
RU2083447C1 (en
Inventor
С.И. Перницкий
С.С. Перницкий
Original Assignee
С.И. Перницкий
С.С. Перницкий
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 С.И. Перницкий, С.С. Перницкий filed Critical С.И. Перницкий
Priority to RU94001670A priority Critical patent/RU2083447C1/en
Publication of RU94001670A publication Critical patent/RU94001670A/en
Application granted granted Critical
Publication of RU2083447C1 publication Critical patent/RU2083447C1/en

Links

Classifications

    • 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
    • B64G1/402—Propellant tanks; Feeding propellants
    • 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)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Navigation (AREA)

Abstract

FIELD: aeronautical engineering. SUBSTANCE: method consists in fuelling the launch vehicle, flight over injection path and separation of payload. Innovation of invention consists in fuelling the launch vehicle with guaranteed amount of fuel for at least one stage which is fully or partially carried in next stage or in payload and is fed to previous stage during flight when required. This invention may be used for any launch vehicle to reduce guaranteed fuel capacity of launch vehicle or to increase fuel capacity of space vehicle injected by launch vehicle. It is good practice to apply this method when it is necessary to increase fuel capacity of space vehicle but mass of vehicle exceeds limiting magnitude the launch vehicle can inject. EFFECT: enhanced reliability.

Claims (1)

Способ выведения полезного груза на орбиту, включающий заправку носителя топливом, полет по траектории выведения и отделение полезного груза отличается тем, что при заправке носителя топливом гарантийный запас топлива по крайней мере одной ступени частично или полностью размещают в последующей ступени или в полезном грузе, а в полете подают его в предыдущую ступень по мире необходимости. Предлагаемое изобретение может быть использовано на любых носителях для уменьшения гарантийного запаса топлива носителя либо для увеличения запаса топлива на выводимом носителем космическом аппарате. Предпочтительной областью использования являются ситуации, когда на космическом аппарате необходимо увеличить запас топлива, но масса аппарата при атом повышается сверх предельной величины массы, которую может вывести носитель.The method of putting payload into orbit, including filling the carrier with fuel, flying along the launch trajectory and separating the payload, differs in that when refueling the carrier with fuel, the guaranteed fuel supply of at least one stage is partially or fully placed in the next stage or in the payload, and the flight serves him to the previous stage in the world of necessity. The present invention can be used on any media to reduce the guaranteed fuel supply of the carrier or to increase the fuel supply on the spacecraft displayed by the carrier. The preferred area of use is situations where it is necessary to increase the fuel supply on the spacecraft, but the mass of the spacecraft at the atom rises above the limit mass that the carrier can bring out.
RU94001670A 1994-01-19 1994-01-19 Method of injection of payload into orbit RU2083447C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94001670A RU2083447C1 (en) 1994-01-19 1994-01-19 Method of injection of payload into orbit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94001670A RU2083447C1 (en) 1994-01-19 1994-01-19 Method of injection of payload into orbit

Publications (2)

Publication Number Publication Date
RU94001670A true RU94001670A (en) 1996-09-27
RU2083447C1 RU2083447C1 (en) 1997-07-10

Family

ID=20151590

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94001670A RU2083447C1 (en) 1994-01-19 1994-01-19 Method of injection of payload into orbit

Country Status (1)

Country Link
RU (1) RU2083447C1 (en)

Also Published As

Publication number Publication date
RU2083447C1 (en) 1997-07-10

Similar Documents

Publication Publication Date Title
US4451017A (en) Three stage rocket vehicle with parallel staging
EA199900900A1 (en) METHOD OF CHANGING THE INCIDENCE AND HEIGHT OF THE ORBIT OF A SPACE AIRCRAFT WITH THE USE OF THE LIMITS OF THE SMALL SUSTAINABILITY
CA2159343A1 (en) A method and an apparatus for spreading warheads
RU94001670A (en) Method of injection of payload into orbit
Bruckner et al. Ram Accelerator direct launch system for space cargo
GB1342067A (en) Method for transporting buoyant gases
RU93043430A (en) METHOD FOR DISPLACING USEFUL LOAD TO ORBIT
TABATA Engineering Test Satellite III-Kiku 4
BUBLITZ History of aeroelasticity in Germany from the beginning to 1945
Sarychev Aerodynamic stabilization system for small satellites
Fahrney Genesis of the Cruise Missile.
Cruddace et al. SPEAR-Small payload ejection and recovery for the Space Shuttle
Rich Space: Back to Mars
McCoy Liquid airbreathing missile fuels: An overview of properties and applications
Green et al. Comparison of the atlas/centaur/surveyor/and igm guidance concepts
Yu et al. An experimental study on the ignition processes of a liquid propellent droplet group
MCSPADDEN High density impulse propellants
RU95109380A (en) Method of destruction of nuclear weapon-carrying satellites, aircraft, war heads of intercontinental rockets and other man-made and natural celestial bodies and device "shield" for its implementation
Roberts OTV impacts and interactions
RU94022030A (en) Method of operation of recoverable space vehicle
Arritt et al. The Aries controlled sounding rocket
Hudson Advanced solar system spaceships
Bushuev et al. Selection of orbital parameters for a satellite with a gyroaerodynamic attitude stabilization system
Bartsev et al. Alternative strategy for space exploration and mastering
Delahais et al. The actions of ESA to prepare for future European Space Transportation Systems