MA61702B1 - Système satellite et véhicule de lancement combiné - Google Patents

Système satellite et véhicule de lancement combiné

Info

Publication number
MA61702B1
MA61702B1 MA61702A MA61702A MA61702B1 MA 61702 B1 MA61702 B1 MA 61702B1 MA 61702 A MA61702 A MA 61702A MA 61702 A MA61702 A MA 61702A MA 61702 B1 MA61702 B1 MA 61702B1
Authority
MA
Morocco
Prior art keywords
tanks
separation
satellite
launch vehicle
emptied
Prior art date
Application number
MA61702A
Other languages
English (en)
Other versions
MA61702A1 (fr
Inventor
Syed Peer Mohamed SHAH KHADRI
Srinath Ravichandran
Original Assignee
Agnikul Cosmos Private Limited
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 Agnikul Cosmos Private Limited filed Critical Agnikul Cosmos Private Limited
Publication of MA61702A1 publication Critical patent/MA61702A1/fr
Publication of MA61702B1 publication Critical patent/MA61702B1/fr

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • B64G1/4021Tank construction; Details thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/002Launch systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • B64G1/4022Arrangements of tanks in or on spacecraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • B64G1/4024Propellant tanks; Feeding propellants refuelling in space
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645Separators
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645Separators
    • B64G1/6459Fluid-actuated
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/605Reservoirs

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Radio Relay Systems (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Automatic Assembly (AREA)
  • Warehouses Or Storage Devices (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Automatic Cycles, And Cycles In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

La présente invention concerne un système satellite et véhicule de lancement combiné. Plus spécifiquement, l'invention concerne le satellite combiné à l'étage supérieur du véhicule de lancement pour fournir un système plus efficace qui comprend une technologie de séparation de réservoir qui permet au système de satellite de détacher les réservoirs qui ont épuisé tout le propergol stocké dans ceux-ci. La séparation du procédé de l'ensemble réservoir est permise par l'utilisation d'un système de séparation de type pneumatique ou collier de serrage Marman ; les trois réservoirs inférieurs (105) sont vidés en premier (202) pendant le processus, suivi de la séparation des réservoirs vidés (203), le carburant étant complètement rempli dans le second ensemble de réservoirs (203). La première paire de réservoirs (103) est ensuite séparée après que le carburant a été vidé (204). De la même façon, la tuyauterie (106) est également séparée avec elle. La séparation des composants utilisés est réalisée ici (205) et le satellite est prêt pour une insertion en orbite (206).
MA61702A 2020-12-15 2021-12-15 Système satellite et véhicule de lancement combiné MA61702B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IN202041054598 2020-12-15
PCT/IN2021/051175 WO2022130407A1 (fr) 2020-12-15 2021-12-15 Système satellite et véhicule de lancement combiné

Publications (2)

Publication Number Publication Date
MA61702A1 MA61702A1 (fr) 2023-09-27
MA61702B1 true MA61702B1 (fr) 2025-05-30

Family

ID=80113524

Family Applications (1)

Application Number Title Priority Date Filing Date
MA61702A MA61702B1 (fr) 2020-12-15 2021-12-15 Système satellite et véhicule de lancement combiné

Country Status (11)

Country Link
US (1) US12466582B2 (fr)
EP (1) EP4263358B1 (fr)
KR (1) KR20230142707A (fr)
AU (1) AU2021404105A1 (fr)
CO (1) CO2023009416A2 (fr)
EC (1) ECSP23053647A (fr)
ES (1) ES3041586T3 (fr)
MA (1) MA61702B1 (fr)
MX (1) MX2023007079A (fr)
WO (1) WO2022130407A1 (fr)
ZA (1) ZA202307107B (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12286243B2 (en) * 2022-05-12 2025-04-29 Maxar Space Llc Stacked spacecraft launch and orbit raising

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4451017A (en) * 1982-09-30 1984-05-29 The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Three stage rocket vehicle with parallel staging
US5217187A (en) * 1983-11-07 1993-06-08 Criswell David R Multi-use launch system
US20090206204A1 (en) * 2008-01-24 2009-08-20 Harold Alvin Rosen Spin-stabilized lander
US20160031571A1 (en) * 2012-07-31 2016-02-04 The Boeing Company Multiple stage tractor propulsion vehicle

Family Cites Families (15)

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Publication number Priority date Publication date Assignee Title
US4231537A (en) 1978-03-22 1980-11-04 Satellite Business Systems Satellite-launch vehicle combination and method
US5242135A (en) * 1990-01-30 1993-09-07 Scott David R Space transfer vehicle and integrated guidance launch system
US5143327A (en) * 1990-08-31 1992-09-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated launch and emergency vehicle system
US5217188A (en) * 1991-04-08 1993-06-08 Trw Inc. Modular solid-propellant launch vehicle and related launch facility
US5927653A (en) * 1996-04-17 1999-07-27 Kistler Aerospace Corporation Two-stage reusable earth-to-orbit aerospace vehicle and transport system
WO2002077660A2 (fr) 2001-03-27 2002-10-03 Space Launch Corporation Systeme d'installation et de correction d'orbite de microsatellites et petits instruments spatiaux
US6968673B1 (en) * 2003-11-14 2005-11-29 Knight Andrew F Cool gas generator and ultra-safe rocket engine
US7137588B2 (en) * 2004-01-06 2006-11-21 United Technologies Corporation Ballistic target defense system and methods
US7780119B2 (en) * 2006-12-11 2010-08-24 Michael David Johnson Modular spacecraft
US9273634B2 (en) * 2011-08-18 2016-03-01 Patrick R. E. Bahn Rocket stage and method of improving an existing rocket stage
US9434485B1 (en) * 2013-01-25 2016-09-06 Stephen C. Lehocki Multi-purpose cargo delivery and space debris removal system
US10589879B2 (en) * 2017-06-07 2020-03-17 Space Systems/Loral, Llc Cross-feeding propellant between stacked spacecraft
KR101833455B1 (ko) 2017-11-15 2018-04-13 동병길 로켓의 연속 점화 구조
CN108052030A (zh) 2018-02-08 2018-05-18 黄君 模块化卫星架构
US11759837B1 (en) * 2018-10-24 2023-09-19 Abl Space Systems Systems and methods for launch vehicle dome manufacturing

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4451017A (en) * 1982-09-30 1984-05-29 The United States Of America As Represented By The Administrator, National Aeronautics And Space Administration Three stage rocket vehicle with parallel staging
US5217187A (en) * 1983-11-07 1993-06-08 Criswell David R Multi-use launch system
US20090206204A1 (en) * 2008-01-24 2009-08-20 Harold Alvin Rosen Spin-stabilized lander
US20160031571A1 (en) * 2012-07-31 2016-02-04 The Boeing Company Multiple stage tractor propulsion vehicle

Also Published As

Publication number Publication date
ECSP23053647A (es) 2023-08-31
CO2023009416A2 (es) 2023-07-31
KR20230142707A (ko) 2023-10-11
AU2021404105A1 (en) 2023-08-03
WO2022130407A1 (fr) 2022-06-23
EP4263358A1 (fr) 2023-10-25
MA61702A1 (fr) 2023-09-27
US12466582B2 (en) 2025-11-11
MX2023007079A (es) 2023-08-25
US20240051685A1 (en) 2024-02-15
EP4263358B1 (fr) 2025-07-23
ES3041586T3 (en) 2025-11-13
EP4263358C0 (fr) 2025-07-23
ZA202307107B (en) 2025-03-26

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