ES2052341T3 - Dispositivo de freno aerodinamico. - Google Patents
Dispositivo de freno aerodinamico.Info
- Publication number
- ES2052341T3 ES2052341T3 ES91400958T ES91400958T ES2052341T3 ES 2052341 T3 ES2052341 T3 ES 2052341T3 ES 91400958 T ES91400958 T ES 91400958T ES 91400958 T ES91400958 T ES 91400958T ES 2052341 T3 ES2052341 T3 ES 2052341T3
- Authority
- ES
- Spain
- Prior art keywords
- fabric
- ring
- brake device
- rigid rings
- tension
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Lifetime
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
- B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
- B64G1/623—Retarding devices, e.g. retrorockets
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
- Woven Fabrics (AREA)
- Valves And Accessory Devices For Braking Systems (AREA)
- Tires In General (AREA)
Abstract
DISPOSITIVO DE FRENADO AERODINAMICO, DESTINADO EN PARTICULAR A LA DECELERACION DE UN OBJETO ESPACIAL QUE PENETRA A GRAN VELOCIDAD EN UNA ATMOSFERA, CONSTITUIDO ESENCIALMENTE DE UN ANILLO CIRCULAR (2) DE TELA, DE FORMA GENERAL VECINA DE LA DE UN TRONCO DE CONO PERO CUYA SECCION POR UN PLANO AXIAL PRESENTA UNA CONCAVIDAD HACIA EL EXTERIOR, Y DE UNA ESTRUCTURA DE SOPORTE (6, 7, 8) CONCEBIDA PARA APLICAR A DICHO ANILLO UNA TENSION DE TRACCION TANGENCIAL EN UN PLANO AXIAL, Y QUE COMPRENDE PREFERENTEMENTE AL MENOS DOS ANILLOS RIGIDOS PARALELOS (6, 7), EN LOS QUE EL ANILLO DE TELA ES TENSADO Y UNAS TRAVIESAS (8) DISPUESTAS PARA MANTENER LA DISTANCIA ENTRE LOS DOS ANILLOS RIGIDOS RESISTIENDO A LOS ESFUERZOS QUE RESULTAN DE LA TENSION DE LA TELA.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR909004807A FR2660908B1 (fr) | 1990-04-13 | 1990-04-13 | Dispositif de freinage aerodynamique. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2052341T3 true ES2052341T3 (es) | 1994-07-01 |
Family
ID=9395772
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES91400958T Expired - Lifetime ES2052341T3 (es) | 1990-04-13 | 1991-04-10 | Dispositivo de freno aerodinamico. |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5108046A (es) |
| EP (1) | EP0453353B1 (es) |
| AT (1) | ATE102564T1 (es) |
| CA (1) | CA2040072C (es) |
| DE (1) | DE69101331T2 (es) |
| ES (1) | ES2052341T3 (es) |
| FR (1) | FR2660908B1 (es) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5201832A (en) * | 1992-03-23 | 1993-04-13 | General Dynamics Corporation, Space Systems Division | Integrated aerospike engine and aerobrake for a spacecraft |
| DE4339052C2 (de) * | 1993-11-16 | 1996-02-15 | Juergen Haro | Container für den Lufttransport |
| FR2728229B1 (fr) * | 1994-12-19 | 1997-03-14 | Centre Nat Etd Spatiales | Bouclier de freinage pour engin spatial et satellite ainsi equipe |
| US6860448B2 (en) * | 2001-09-05 | 2005-03-01 | Omnitek Partners, Llc | Deployable projectiles |
| EP1540264B1 (de) * | 2002-09-13 | 2010-06-09 | Diehl BGT Defence GmbH & Co.KG | Bremseinrichtung für ein bahnkorrigierbares drallstabilisiertes artillerieprojektil |
| US7219859B2 (en) * | 2005-04-01 | 2007-05-22 | Spacehab, Incorporated | Multipurpose modular spacecraft |
| US8469314B2 (en) * | 2010-02-03 | 2013-06-25 | The United States Of America, As Represented By The Secretary Of The Navy | Technique for de-orbiting small debris from the near-earth space environment |
| US9174738B1 (en) * | 2013-04-14 | 2015-11-03 | Google Inc. | Drag disk, small |
| US9522747B2 (en) * | 2014-06-03 | 2016-12-20 | Analytical Mechanics Associates, Inc. | Inflatable deceleration apparatus |
| US10081446B2 (en) * | 2015-03-11 | 2018-09-25 | William C. Stone | System for emergency crew return and down-mass from orbit |
| CN105584645B (zh) * | 2016-01-13 | 2017-08-04 | 北京空间技术研制试验中心 | 半刚性机械展开进入减速着陆装置 |
| US11420775B2 (en) * | 2018-10-04 | 2022-08-23 | The Aerospace Corporation | Systems and methods for deploying a deorbiting device |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3118636A (en) * | 1959-01-08 | 1964-01-21 | Avco Mfg Corp | Space vehicle |
| US3433435A (en) * | 1966-07-25 | 1969-03-18 | Gen Electric | Tension string drag structures for planetary entry vehicle |
| US3405887A (en) * | 1966-10-10 | 1968-10-15 | Nasa Usa | Ring wing tension vehicle |
| US3888175A (en) * | 1966-10-18 | 1975-06-10 | Us Army | Mechanical stabilizer |
| US3604667A (en) * | 1968-11-26 | 1971-09-14 | Martin Marietta Corp | Planetary lander |
| US4817895A (en) * | 1985-06-18 | 1989-04-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Aerobraking orbital transfer vehicle |
| DE3643293A1 (de) * | 1986-12-18 | 1988-06-30 | Rheinmetall Gmbh | Drallstabilisiertes traegergeschoss mit mindestens zwei submunitionsgeschossen |
| DE3643294A1 (de) * | 1986-12-18 | 1988-06-23 | Rheinmetall Gmbh | Geschoss |
| US4903918A (en) * | 1987-05-28 | 1990-02-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Raked circular-cone aerobraking orbital transfer vehicle |
| US4832288A (en) * | 1987-07-23 | 1989-05-23 | Aerospace Recovery System, Inc. | Recovery system |
| DE3830650A1 (de) * | 1988-09-09 | 1990-03-15 | Ohb Opto Elektronik Hydraulik | Brems- und stabilisierungssystem fuer flugkoerper in supersonischen geschwindigkeitsbereichen |
-
1990
- 1990-04-13 FR FR909004807A patent/FR2660908B1/fr not_active Expired - Fee Related
-
1991
- 1991-04-04 US US07/680,359 patent/US5108046A/en not_active Expired - Lifetime
- 1991-04-09 CA CA002040072A patent/CA2040072C/en not_active Expired - Fee Related
- 1991-04-10 EP EP91400958A patent/EP0453353B1/fr not_active Expired - Lifetime
- 1991-04-10 ES ES91400958T patent/ES2052341T3/es not_active Expired - Lifetime
- 1991-04-10 AT AT91400958T patent/ATE102564T1/de not_active IP Right Cessation
- 1991-04-10 DE DE69101331T patent/DE69101331T2/de not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| FR2660908B1 (fr) | 1994-09-09 |
| US5108046A (en) | 1992-04-28 |
| ATE102564T1 (de) | 1994-03-15 |
| CA2040072A1 (en) | 1991-10-14 |
| DE69101331T2 (de) | 1994-06-16 |
| EP0453353B1 (fr) | 1994-03-09 |
| EP0453353A1 (fr) | 1991-10-23 |
| FR2660908A1 (fr) | 1991-10-18 |
| DE69101331D1 (de) | 1994-04-14 |
| CA2040072C (en) | 1997-09-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
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