GB922560A - Improvements in or relating to rocket motors - Google Patents
Improvements in or relating to rocket motorsInfo
- Publication number
- GB922560A GB922560A GB2725758A GB2725758A GB922560A GB 922560 A GB922560 A GB 922560A GB 2725758 A GB2725758 A GB 2725758A GB 2725758 A GB2725758 A GB 2725758A GB 922560 A GB922560 A GB 922560A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cap
- lugs
- engage
- rocket
- aug
- 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
-
- 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
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/38—Safety devices, e.g. to prevent accidental ignition
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H29/00—Drive mechanisms for toys in general
- A63H29/10—Driving mechanisms actuated by flowing media
- A63H29/16—Driving mechanisms actuated by flowing media by steam or compressed air
Abstract
922,560. Rocket motors. D. SEBEL & CO. Ltd. Aug. 24, 1959 [Aug. 25, 1958], No. 27257/58. Class 9 (2). Relates to a rocket motor as described in Specification 688,838 having an end cap 4 closing the rocket chamber 1 and a frangible diaphragm 17 clamped between a back plate 10 and the cap to close aligned pressure-relief apertures 9, 11. The back plate is of such a diameter that it is positively held by the cap and, to align the passages 9, 11, the plate has an opening 12 to engage a pin 13 projecting from the cap. To secure the cap to the casing 1, lugs 20 within the cap engage lugs 19 on the casing, the lugs being provided with cam surfaces which will not engage if the diaphragm is too thick. Screw-threading may be used in place of the lugs.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2725758A GB922560A (en) | 1958-08-25 | 1958-08-25 | Improvements in or relating to rocket motors |
FR39697A FR1233415A (en) | 1958-08-25 | 1959-08-25 | Improvements to jet engines, especially for model aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2725758A GB922560A (en) | 1958-08-25 | 1958-08-25 | Improvements in or relating to rocket motors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB922560A true GB922560A (en) | 1963-04-03 |
Family
ID=10256635
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2725758A Expired GB922560A (en) | 1958-08-25 | 1958-08-25 | Improvements in or relating to rocket motors |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1233415A (en) |
GB (1) | GB922560A (en) |
-
1958
- 1958-08-25 GB GB2725758A patent/GB922560A/en not_active Expired
-
1959
- 1959-08-25 FR FR39697A patent/FR1233415A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR1233415A (en) | 1960-10-12 |
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