GB2162623B - A mechanism for aerodynamic deceleration and a body including such a mechanism - Google Patents
A mechanism for aerodynamic deceleration and a body including such a mechanismInfo
- Publication number
- GB2162623B GB2162623B GB08515032A GB8515032A GB2162623B GB 2162623 B GB2162623 B GB 2162623B GB 08515032 A GB08515032 A GB 08515032A GB 8515032 A GB8515032 A GB 8515032A GB 2162623 B GB2162623 B GB 2162623B
- Authority
- GB
- United Kingdom
- Prior art keywords
- body including
- aerodynamic deceleration
- aerodynamic
- deceleration
- 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
Links
Classifications
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/004—Mounting transducers, e.g. provided with mechanical moving or orienting device
- G10K11/006—Transducer mounting in underwater equipment, e.g. sonobuoys
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Braking Arrangements (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19843422231 DE3422231A1 (en) | 1984-06-15 | 1984-06-15 | DEVICE FOR AERODYNAMICALLY BRAKING THE ROTATIONAL MOVEMENT OF A BODY |
DE19843422206 DE3422206A1 (en) | 1984-06-15 | 1984-06-15 | Underwater sound transducer, particularly for low frequencies |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8515032D0 GB8515032D0 (en) | 1985-07-17 |
GB2162623A GB2162623A (en) | 1986-02-05 |
GB2162623B true GB2162623B (en) | 1988-08-10 |
Family
ID=25822136
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08515032A Expired GB2162623B (en) | 1984-06-15 | 1985-06-13 | A mechanism for aerodynamic deceleration and a body including such a mechanism |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2162623B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3741779A1 (en) * | 1987-12-10 | 1989-06-22 | Autoflug Gmbh | BRAKE DEVICE FOR ROTATING MISSILE |
GB9015445D0 (en) * | 1990-07-13 | 1991-02-20 | Royal Ordnance Plc | Projectile surveillance apparatus |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB745252A (en) * | 1953-07-29 | 1956-02-22 | Ml Aviation Co Ltd | Improvements relating to rocket propelled projectiles |
FR1506571A (en) * | 1966-11-10 | 1967-12-22 | Matra Engins | Airplane bomb |
DE2609932C2 (en) * | 1976-03-10 | 1984-04-05 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Folding tail for missiles |
US4351499A (en) * | 1979-09-24 | 1982-09-28 | General Dynamics | Double fabric, retractable, self-erecting wing for missle |
US4350315A (en) * | 1980-05-27 | 1982-09-21 | The United Staates Of America As Represented By The Secretary Of The Army | Device to de-spin objects with very high spin |
US4411398A (en) * | 1981-04-20 | 1983-10-25 | General Dynamics, Pomona Division | Double fabric retractable wing construction |
DE3403573A1 (en) * | 1983-11-09 | 1985-08-08 | Diehl GmbH & Co, 8500 Nürnberg | BULLET WITH FOLD-OUT WINGS |
-
1985
- 1985-06-13 GB GB08515032A patent/GB2162623B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2162623A (en) | 1986-02-05 |
GB8515032D0 (en) | 1985-07-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |