DE1069505B - - Google Patents
Info
- Publication number
- DE1069505B DE1069505B DENDAT1069505D DE1069505DA DE1069505B DE 1069505 B DE1069505 B DE 1069505B DE NDAT1069505 D DENDAT1069505 D DE NDAT1069505D DE 1069505D A DE1069505D A DE 1069505DA DE 1069505 B DE1069505 B DE 1069505B
- Authority
- DE
- Germany
- Prior art keywords
- projectile
- rocket
- gun
- launch pad
- ice
- 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.)
- Pending
Links
- 239000000203 mixture Substances 0.000 claims description 2
- 239000003380 propellant Substances 0.000 claims description 2
- 235000015842 Hesperis Nutrition 0.000 claims 1
- 235000012633 Iberis amara Nutrition 0.000 claims 1
- 230000006378 damage Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
Raketengeschoß, welches durch das Gasluftgemisch eines Treibstoffes aus einer geschützartigen Abschußrampe getrieben Wird Bei Raketengeschossen, die aus einer geschÜtzartigen Abschußrampe getrieben werden, besteht wegen der auf diese Weise zu erzielenden sehr hohen Geschwindigkeiten eine erhöhte Erwärmungs- bzw. Verbrennungsgefahr, die nicht nur zur Zerstörung von Inneneinrichtungen bzw. zur Schädigung der gegebenenfalls im Raketengesehoß untergebrachten Bemannung, sondern ebenfalls zur Verbrennung des Geschosses selbst führen kann. Die unzulässig hohe Erwärmung kann sowohl durch die Reibung des Geschosses im Geschützrohr der Abschußrampe als auch beim Durchtritt desselben durch die Atmosphäre während des Aufstieges bzw. während der Rückkehr zur Erde auftreten.Rocket projectile, which is caused by the gas-air mixture of a propellant propelled from a gun-like launch pad be driven from a gun-like launch pad, exists because of this Way to achieve very high speeds an increased heating resp. Risk of burns, which not only leads to the destruction of interior fittings or to Damage to the crews possibly accommodated in the rocket shell, but rather can also burn the projectile itself. The unacceptably high Heating can be caused by the friction of the projectile in the gun barrel of the launch pad as well as when it passes through the atmosphere during the ascent or occur during the return to earth.
Erfindungsgemäß wird diese Gefahr dadurch beseitigt, daß das Geschoß mit einem eisgekühlten Mantel umgeben ist, der gegebenenfalls kurz vor dem Abschuß um dasselbe gelegt wird.According to the invention, this risk is eliminated in that the projectile is surrounded with an ice-cold coat, which may be shortly before the launch around the same thing.
Claims (1)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1069505B true DE1069505B (en) | 1959-11-19 |
Family
ID=594610
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DENDAT1069505D Pending DE1069505B (en) |
Country Status (1)
| Country | Link |
|---|---|
| DE (1) | DE1069505B (en) |
-
0
- DE DENDAT1069505D patent/DE1069505B/de active Pending
Non-Patent Citations (1)
| Title |
|---|
| None * |
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