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EP2455704A3 - Missile with a skin having an ablation layer thereon - Google Patents

Missile with a skin having an ablation layer thereon Download PDF

Info

Publication number
EP2455704A3
EP2455704A3 EP11008941.4A EP11008941A EP2455704A3 EP 2455704 A3 EP2455704 A3 EP 2455704A3 EP 11008941 A EP11008941 A EP 11008941A EP 2455704 A3 EP2455704 A3 EP 2455704A3
Authority
EP
European Patent Office
Prior art keywords
missile
ablation layer
skin
matrix material
flight
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.)
Granted
Application number
EP11008941.4A
Other languages
German (de)
French (fr)
Other versions
EP2455704A2 (en
EP2455704B1 (en
Inventor
Peter Gerd Fisch
Gerd Elsner
Rainer Hezel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Publication of EP2455704A2 publication Critical patent/EP2455704A2/en
Publication of EP2455704A3 publication Critical patent/EP2455704A3/en
Application granted granted Critical
Publication of EP2455704B1 publication Critical patent/EP2455704B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/34—Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/25—Web or sheet containing structurally defined element or component and including a second component containing structurally defined particles
    • Y10T428/252—Glass or ceramic [i.e., fired or glazed clay, cement, etc.] [porcelain, quartz, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)
  • Paints Or Removers (AREA)

Abstract

Die Erfindung geht aus von einem Flugkörper (2) mit einer Außenhülle (12) und einer darauf aufgebrachten Außenbeschichtung in Form einer Ablationsschicht (18), die ein zur zumindest teilweisen Zersetzung während eines Flugs vorgesehenes Matrixmaterial (24) enthält.The invention relates to a missile (2) having an outer shell (12) and an outer coating applied thereto in the form of an ablation layer (18) which contains a matrix material (24) provided for at least partial decomposition during flight.

Um den Flugkörper auch nach einem Flug mit einer Geschwindigkeit oberhalb 1000 m/s zuverlässig einsatzbereit zu halten, wird vorgeschlagen, dass im Matrixmaterial (24) Glashohlkörper (26) eingebettet sind.

Figure imgaf001
In order to keep the missile reliably ready for use even after a flight at a speed above 1000 m / s, it is proposed that glass hollow bodies (26) be embedded in the matrix material (24).
Figure imgaf001
EP11008941.4A 2010-11-17 2011-11-10 Missile with a skin having an ablation layer thereon Active EP2455704B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010051752A DE102010051752A1 (en) 2010-11-17 2010-11-17 Missile with an outer shell and an ablation layer applied thereon

Publications (3)

Publication Number Publication Date
EP2455704A2 EP2455704A2 (en) 2012-05-23
EP2455704A3 true EP2455704A3 (en) 2014-07-16
EP2455704B1 EP2455704B1 (en) 2016-01-27

Family

ID=44992489

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11008941.4A Active EP2455704B1 (en) 2010-11-17 2011-11-10 Missile with a skin having an ablation layer thereon

Country Status (3)

Country Link
US (1) US20120121892A1 (en)
EP (1) EP2455704B1 (en)
DE (1) DE102010051752A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2496090C1 (en) * 2012-05-11 2013-10-20 Николай Борисович Болотин Anti-aircraft missile and liquid-propellant rocket
DE102017007059B4 (en) 2017-07-26 2021-04-01 Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr Method for producing a pipe section of a missile outer shell and a pipe section of a missile outer shell
CN112177697B (en) * 2020-09-09 2022-02-22 西安交通大学 Thermal protection coupling open Brayton power generation system based on thermal decomposition reaction
JP2023074181A (en) * 2021-11-17 2023-05-29 三菱重工業株式会社 Heat-resistant structure of flight body and method for manufacturing the heat-resistant structure of flight body
EP4649279A1 (en) * 2023-01-09 2025-11-19 MBDA UK Limited Missile structure
EP4397938A1 (en) * 2023-01-09 2024-07-10 MBDA UK Limited Missile structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4031059A (en) * 1974-01-21 1977-06-21 Martin Marietta Corporation Low density ablator compositions
US4077921A (en) * 1977-01-19 1978-03-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Sprayable low density ablator and application process
US4837250A (en) * 1987-07-23 1989-06-06 Usbi Booster Production Company, Inc. Trowelable ablative coating composition and method of use
US5661198A (en) * 1993-09-27 1997-08-26 Nissan Motor Co., Ltd. Ablator compositions
EP1493788A1 (en) * 2003-06-25 2005-01-05 United Technologies Corporation Silicone-cork ablative material

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5457471A (en) * 1984-09-10 1995-10-10 Hughes Missile Systems Company Adaptively ablatable radome
US4753169A (en) * 1985-12-23 1988-06-28 General Dynamics, Pomona Division Ablating electromagnetic shield sheath
DE4132234C2 (en) * 1991-09-27 1997-05-07 Rheinmetall Ind Ag Balancing projectile
US20040018309A1 (en) * 2002-07-25 2004-01-29 Carrier Corporation Furnace parts protected by thermally and chemically resistant coatings
US20100112260A1 (en) * 2006-09-11 2010-05-06 Jagdish Ramaniel Patel Thermal insulating material

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4031059A (en) * 1974-01-21 1977-06-21 Martin Marietta Corporation Low density ablator compositions
US4077921A (en) * 1977-01-19 1978-03-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Sprayable low density ablator and application process
US4837250A (en) * 1987-07-23 1989-06-06 Usbi Booster Production Company, Inc. Trowelable ablative coating composition and method of use
US5661198A (en) * 1993-09-27 1997-08-26 Nissan Motor Co., Ltd. Ablator compositions
EP1493788A1 (en) * 2003-06-25 2005-01-05 United Technologies Corporation Silicone-cork ablative material

Also Published As

Publication number Publication date
DE102010051752A1 (en) 2012-05-24
EP2455704A2 (en) 2012-05-23
EP2455704B1 (en) 2016-01-27
US20120121892A1 (en) 2012-05-17

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