DE1231486B - Raketenschubvorrichtung fuer einen Schleudersitz in Flugzeugen - Google Patents
Raketenschubvorrichtung fuer einen Schleudersitz in FlugzeugenInfo
- Publication number
- DE1231486B DE1231486B DES88637A DES0088637A DE1231486B DE 1231486 B DE1231486 B DE 1231486B DE S88637 A DES88637 A DE S88637A DE S0088637 A DES0088637 A DE S0088637A DE 1231486 B DE1231486 B DE 1231486B
- Authority
- DE
- Germany
- Prior art keywords
- plates
- propellant
- housing
- rocket
- stack
- 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
Links
- 239000003380 propellant Substances 0.000 claims description 41
- 239000000446 fuel Substances 0.000 claims description 23
- 239000000567 combustion gas Substances 0.000 claims description 8
- 125000006850 spacer group Chemical group 0.000 claims description 4
- 239000004449 solid propellant Substances 0.000 claims description 3
- 239000007789 gas Substances 0.000 description 11
- 238000002485 combustion reaction Methods 0.000 description 10
- 238000010304 firing Methods 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- 239000000843 powder Substances 0.000 description 4
- 238000003860 storage Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 239000004020 conductor Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- IOMMMLWIABWRKL-WUTDNEBXSA-N nazartinib Chemical compound C1N(C(=O)/C=C/CN(C)C)CCCC[C@H]1N1C2=C(Cl)C=CC=C2N=C1NC(=O)C1=CC=NC(C)=C1 IOMMMLWIABWRKL-WUTDNEBXSA-N 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000003779 heat-resistant material Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000037452 priming Effects 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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
- F02K9/30—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants with the propulsion gases exhausting through a plurality of nozzles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/10—Ejector seats
-
- 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
- F02K9/10—Shape or structure of solid propellant charges
- F02K9/14—Shape or structure of solid propellant charges made from sheet-like materials, e.g. of carpet-roll type, of layered structure
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Aviation & Aerospace Engineering (AREA)
- Testing Of Engines (AREA)
- Jet Pumps And Other Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE1343562 | 1962-12-13 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE1231486B true DE1231486B (de) | 1966-12-29 |
DE1231486C2 DE1231486C2 (en:Method) | 1967-07-13 |
Family
ID=20297406
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DES88637A Granted DE1231486B (de) | 1962-12-13 | 1963-12-09 | Raketenschubvorrichtung fuer einen Schleudersitz in Flugzeugen |
Country Status (5)
Country | Link |
---|---|
AT (1) | AT247161B (en:Method) |
CH (1) | CH407765A (en:Method) |
DE (1) | DE1231486B (en:Method) |
GB (1) | GB1010709A (en:Method) |
NL (1) | NL301658A (en:Method) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0013209A1 (fr) * | 1978-12-28 | 1980-07-09 | Societe Nationale Des Poudres Et Explosifs | Chargement pyrotechnique à faible durée de combustion comprenant des plaques de propergol inclinées et des déflecteurs, propulseur utilisant un tel chargement et plaque de propergol à utiliser dans un tel chargement |
DE3416736A1 (de) * | 1984-05-07 | 1985-11-14 | Dynamit Nobel Ag, 5210 Troisdorf | Treibladungsanzuender |
RU2805347C1 (ru) * | 2022-12-01 | 2023-10-16 | Акционерное общество "Корпорация "Московский институт теплотехники" (АО "Корпорация "МИТ") | Двухсопловой ракетный двигатель твердого топлива (РДТТ) с многошашечным зарядом |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102005049704B4 (de) * | 2005-01-24 | 2011-03-17 | Issa Orans | Rettungssystem zur Opferreduzierung bei Hubschrauberabstürzen |
WO2010018561A1 (en) * | 2008-08-13 | 2010-02-18 | Chibbi Naaman | Helicopter with ejection seat |
CN105109443A (zh) * | 2015-08-31 | 2015-12-02 | 唐慧华 | 多点阵列布控防倾斜装置 |
CN105034886A (zh) * | 2015-08-31 | 2015-11-11 | 唐慧华 | 带有报警按钮的多功能座椅 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434652A (en) * | 1944-03-01 | 1948-01-20 | Usa | Igniter |
US2488154A (en) * | 1944-10-17 | 1949-11-15 | Us Sec War | Strip propellant for rocket projectiles |
US2712283A (en) * | 1944-07-20 | 1955-07-05 | Golden Sidney | Propellent assembly for jet propelled device |
US2918005A (en) * | 1956-10-31 | 1959-12-22 | Schecter George | Sheet propellant |
FR1311661A (fr) * | 1962-01-19 | 1962-12-07 | Perfectionnements apportés aux dispositifs pour l'éjection d'une masse hors d'un engin |
-
0
- NL NL301658D patent/NL301658A/xx unknown
-
1963
- 1963-12-09 DE DES88637A patent/DE1231486B/de active Granted
- 1963-12-10 CH CH1508263A patent/CH407765A/de unknown
- 1963-12-10 AT AT987963A patent/AT247161B/de active
- 1963-12-13 GB GB4932563A patent/GB1010709A/en not_active Expired
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434652A (en) * | 1944-03-01 | 1948-01-20 | Usa | Igniter |
US2712283A (en) * | 1944-07-20 | 1955-07-05 | Golden Sidney | Propellent assembly for jet propelled device |
US2488154A (en) * | 1944-10-17 | 1949-11-15 | Us Sec War | Strip propellant for rocket projectiles |
US2918005A (en) * | 1956-10-31 | 1959-12-22 | Schecter George | Sheet propellant |
FR1311661A (fr) * | 1962-01-19 | 1962-12-07 | Perfectionnements apportés aux dispositifs pour l'éjection d'une masse hors d'un engin |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0013209A1 (fr) * | 1978-12-28 | 1980-07-09 | Societe Nationale Des Poudres Et Explosifs | Chargement pyrotechnique à faible durée de combustion comprenant des plaques de propergol inclinées et des déflecteurs, propulseur utilisant un tel chargement et plaque de propergol à utiliser dans un tel chargement |
DE3416736A1 (de) * | 1984-05-07 | 1985-11-14 | Dynamit Nobel Ag, 5210 Troisdorf | Treibladungsanzuender |
US4669383A (en) * | 1984-05-07 | 1987-06-02 | Dynamit Nobel Aktiengesellschaft | Propellant charge igniter |
RU2805347C1 (ru) * | 2022-12-01 | 2023-10-16 | Акционерное общество "Корпорация "Московский институт теплотехники" (АО "Корпорация "МИТ") | Двухсопловой ракетный двигатель твердого топлива (РДТТ) с многошашечным зарядом |
Also Published As
Publication number | Publication date |
---|---|
NL301658A (en:Method) | |
DE1231486C2 (en:Method) | 1967-07-13 |
GB1010709A (en) | 1965-11-24 |
AT247161B (de) | 1966-05-25 |
CH407765A (de) | 1966-02-15 |
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