ECSP23053647A - Un vehiculo de lanzamiento combinado y sistema de satelite - Google Patents
Un vehiculo de lanzamiento combinado y sistema de sateliteInfo
- Publication number
- ECSP23053647A ECSP23053647A ECSENADI202353647A ECDI202353647A ECSP23053647A EC SP23053647 A ECSP23053647 A EC SP23053647A EC SENADI202353647 A ECSENADI202353647 A EC SENADI202353647A EC DI202353647 A ECDI202353647 A EC DI202353647A EC SP23053647 A ECSP23053647 A EC SP23053647A
- Authority
- EC
- Ecuador
- 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 presente invención se refiere a un sistema combinado de vehículo de lanzamiento y satélite. Más concretamente se refiere al satélite combinado con la etapa superior del vehículo de lanzamiento para proporcionar un sistema más eficiente que incluye tecnología de separación de tanques que permite al sistema de satélite desprenderse de los tanques que han agotado todos los propulsantes almacenados en ellos. El método de separación del conjunto de tanques se habilita mediante el uso de un sistema de separación de tipo banda merman o neumático; en el que los tres tanques inferiores (105) se vacían primero (202) durante el proceso, seguido de la separación de los tanques vaciados (203) aquí el combustible se llena completamente en el segundo conjunto de tanques (203). A continuación, se separa el primer par de depósitos (103) una vez vaciado el combustible (204). Del mismo modo, también se separan los conductos de fontanería (106). La separación de los componentes utilizados se consigue aquí (205) y el satélite está listo para su inserción en órbita (206).
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IN202041054598 | 2020-12-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ECSP23053647A true ECSP23053647A (es) | 2023-08-31 |
Family
ID=80113524
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ECSENADI202353647A ECSP23053647A (es) | 2020-12-15 | 2023-07-14 | Un vehiculo de lanzamiento combinado y sistema de satelite |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US12466582B2 (es) |
| EP (1) | EP4263358B1 (es) |
| KR (1) | KR20230142707A (es) |
| AU (1) | AU2021404105A1 (es) |
| CO (1) | CO2023009416A2 (es) |
| EC (1) | ECSP23053647A (es) |
| ES (1) | ES3041586T3 (es) |
| MA (1) | MA61702B1 (es) |
| MX (1) | MX2023007079A (es) |
| WO (1) | WO2022130407A1 (es) |
| ZA (1) | ZA202307107B (es) |
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 |
Family Cites Families (19)
| 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 |
| 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 |
| 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 (en) | 2001-03-27 | 2002-10-03 | Space Launch Corporation | A system for the delivery and orbital maintenance of micro satellites and small space-based instruments |
| 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 |
| CA2706719A1 (en) | 2008-01-24 | 2009-07-30 | Harold Rosen | Spin-stabilized lander |
| US9273634B2 (en) * | 2011-08-18 | 2016-03-01 | Patrick R. E. Bahn | Rocket stage and method of improving an existing rocket stage |
| US9114892B1 (en) * | 2012-07-31 | 2015-08-25 | The Boeing Company | Multiple stage tractor propulsion vehicle |
| 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/en active Active
- 2021-12-15 WO PCT/IN2021/051175 patent/WO2022130407A1/en 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
Also Published As
| Publication number | Publication date |
|---|---|
| CO2023009416A2 (es) | 2023-07-31 |
| KR20230142707A (ko) | 2023-10-11 |
| AU2021404105A1 (en) | 2023-08-03 |
| WO2022130407A1 (en) | 2022-06-23 |
| EP4263358A1 (en) | 2023-10-25 |
| MA61702A1 (fr) | 2023-09-27 |
| MA61702B1 (fr) | 2025-05-30 |
| US12466582B2 (en) | 2025-11-11 |
| MX2023007079A (es) | 2023-08-25 |
| US20240051685A1 (en) | 2024-02-15 |
| EP4263358B1 (en) | 2025-07-23 |
| ES3041586T3 (en) | 2025-11-13 |
| EP4263358C0 (en) | 2025-07-23 |
| ZA202307107B (en) | 2025-03-26 |
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