MA61702B1 - Système satellite et véhicule de lancement combiné - Google Patents
Système satellite et véhicule de lancement combinéInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
-
- 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
- B64G1/4021—Tank construction; Details thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
-
- 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
-
- 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
- B64G1/4022—Arrangements of tanks in or on spacecraft
-
- 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
- B64G1/4024—Propellant tanks; Feeding propellants refuelling in space
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/645—Separators
- B64G1/6459—Fluid-actuated
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/605—Reservoirs
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).
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)
| 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)
| 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)
| 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 |
-
2021
- 2021-12-15 MA MA61702A patent/MA61702B1/fr unknown
- 2021-12-15 US US18/267,657 patent/US12466582B2/en active Active
- 2021-12-15 AU AU2021404105A patent/AU2021404105A1/en active Pending
- 2021-12-15 MX MX2023007079A patent/MX2023007079A/es unknown
- 2021-12-15 ES ES21847781T patent/ES3041586T3/es active Active
- 2021-12-15 EP EP21847781.8A patent/EP4263358B1/fr active Active
- 2021-12-15 WO PCT/IN2021/051175 patent/WO2022130407A1/fr not_active Ceased
- 2021-12-15 KR KR1020237024238A patent/KR20230142707A/ko active Pending
-
2023
- 2023-07-14 EC ECSENADI202353647A patent/ECSP23053647A/es unknown
- 2023-07-14 ZA ZA2023/07107A patent/ZA202307107B/en unknown
- 2023-07-14 CO CONC2023/0009416A patent/CO2023009416A2/es unknown
Patent Citations (4)
| 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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