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RU2007111070A - ROCKET - Google Patents

ROCKET Download PDF

Info

Publication number
RU2007111070A
RU2007111070A RU2007111070/11A RU2007111070A RU2007111070A RU 2007111070 A RU2007111070 A RU 2007111070A RU 2007111070/11 A RU2007111070/11 A RU 2007111070/11A RU 2007111070 A RU2007111070 A RU 2007111070A RU 2007111070 A RU2007111070 A RU 2007111070A
Authority
RU
Russia
Prior art keywords
rocket
nozzles
tank
accordion
offset
Prior art date
Application number
RU2007111070/11A
Other languages
Russian (ru)
Other versions
RU2340517C2 (en
Inventor
ев Александр Михайлович Гульт (RU)
Александр Михайлович Гультяев
Original Assignee
ев Александр Михайлович Гульт (RU)
Александр Михайлович Гультяев
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 ев Александр Михайлович Гульт (RU), Александр Михайлович Гультяев filed Critical ев Александр Михайлович Гульт (RU)
Priority to RU2007111070/11A priority Critical patent/RU2340517C2/en
Publication of RU2007111070A publication Critical patent/RU2007111070A/en
Application granted granted Critical
Publication of RU2340517C2 publication Critical patent/RU2340517C2/en

Links

Landscapes

  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Details Of Rigid Or Semi-Rigid Containers (AREA)
  • Jet Pumps And Other Pumps (AREA)

Claims (2)

1. Ракета состоит из корпуса, бака, крыльев сопел, отличающаяся тем, что бак имеет форму круглой гармошки, а сопла имеют разные выходные отверстия, которые по мере удаления от оси ракеты увеличиваются.1. The rocket consists of a body, tank, nozzle wings, characterized in that the tank has the shape of a round accordion, and the nozzles have different outlet openings, which increase with distance from the axis of the rocket. 2. Ракета по п.1, отличающаяся тем, что сопла расположены в конусном варианте со смещением.2. The rocket according to claim 1, characterized in that the nozzles are located in a conical embodiment with an offset.
RU2007111070/11A 2007-03-26 2007-03-26 Rocket RU2340517C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2007111070/11A RU2340517C2 (en) 2007-03-26 2007-03-26 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2007111070/11A RU2340517C2 (en) 2007-03-26 2007-03-26 Rocket

Publications (2)

Publication Number Publication Date
RU2007111070A true RU2007111070A (en) 2007-07-10
RU2340517C2 RU2340517C2 (en) 2008-12-10

Family

ID=38316478

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007111070/11A RU2340517C2 (en) 2007-03-26 2007-03-26 Rocket

Country Status (1)

Country Link
RU (1) RU2340517C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2420432C2 (en) * 2010-06-28 2011-06-10 Александр Михайлович Гультяев Spaceship

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3232560A (en) * 1963-02-25 1966-02-01 Aerojet General Co Recoverable space vehicle
US4964340A (en) * 1988-10-07 1990-10-23 Space Services, Incorporated Overlapping stage burn for multistage launch vehicles
RU2005633C1 (en) * 1992-01-27 1994-01-15 Панов Сергей Александрович Fuel tank
RU2088787C1 (en) * 1994-03-28 1997-08-27 Аркадий Алексеевич Бахмутов Multistage rocket
RU2006117937A (en) * 2006-05-24 2006-09-20 ев Александр Михайлович Гульт (RU) DEFORMING AIRCRAFT

Also Published As

Publication number Publication date
RU2340517C2 (en) 2008-12-10

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