GB1266266A - - Google Patents
Info
- Publication number
- GB1266266A GB1266266A GB1266266DA GB1266266A GB 1266266 A GB1266266 A GB 1266266A GB 1266266D A GB1266266D A GB 1266266DA GB 1266266 A GB1266266 A GB 1266266A
- Authority
- GB
- United Kingdom
- Prior art keywords
- burning
- compositions
- block
- propellant
- line
- 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
- 239000000203 mixture Substances 0.000 abstract 6
- 239000003380 propellant Substances 0.000 abstract 3
- 235000015842 Hesperis Nutrition 0.000 abstract 1
- 235000012633 Iberis amara Nutrition 0.000 abstract 1
- 230000001133 acceleration Effects 0.000 abstract 1
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 238000009413 insulation Methods 0.000 abstract 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
- F02K9/10—Shape or structure of solid propellant charges
- F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/68—Line-carrying missiles, e.g. for life-saving
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Testing Of Engines (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Compression Or Coding Systems Of Tv Signals (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19691943529 DE1943529C2 (de) | 1969-08-27 | 1969-08-27 | Leinenwurfrakete |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1266266A true GB1266266A (https=) | 1972-03-08 |
Family
ID=5743901
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1266266D Expired GB1266266A (https=) | 1969-08-27 | 1970-08-24 |
Country Status (6)
| Country | Link |
|---|---|
| BE (1) | BE755381A (https=) |
| DE (1) | DE1943529C2 (https=) |
| FR (1) | FR2064803A5 (https=) |
| GB (1) | GB1266266A (https=) |
| NO (1) | NO128365B (https=) |
| SE (1) | SE385242B (https=) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001038170A1 (en) * | 1999-11-23 | 2001-05-31 | Technanogy, Llc | Single-stage-to-orbit rocket |
| WO2001038711A1 (en) * | 1999-11-23 | 2001-05-31 | Technanogy, Llc | End-burning rocket motor |
| RU2327052C2 (ru) * | 2006-07-26 | 2008-06-20 | Федеральное государственное унитарное предприятие "Федеральный центр двойных технологий "Союз" (ФГУП "ФЦДТ "Союз") | Способ газодинамической стабилизации давления в камере модельного двигателя с зарядами твердого ракетного топлива с высокой чувствительностью скорости горения от давления |
| RU2376490C1 (ru) * | 2008-06-11 | 2009-12-20 | Федеральное государственное унитарное предприятие "Федеральный центр двойных технологий "Союз" (ФГУП "ФЦДТ" "Союз") | Способ безынерционного определения предела минимального давления устойчивости рабочего процесса трду |
| CN111268066A (zh) * | 2020-02-27 | 2020-06-12 | 北京凌天智能装备集团股份有限公司 | 一种多功能气动抛投器 |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NO930775L (no) * | 1993-03-03 | 1994-09-05 | Andersen Stein Petter | Bergingssystem for ubemannede fartöyer |
-
0
- BE BE755381D patent/BE755381A/xx unknown
-
1969
- 1969-08-27 DE DE19691943529 patent/DE1943529C2/de not_active Expired
-
1970
- 1970-08-24 GB GB1266266D patent/GB1266266A/en not_active Expired
- 1970-08-26 NO NO325170A patent/NO128365B/no unknown
- 1970-08-26 FR FR7031239A patent/FR2064803A5/fr not_active Expired
- 1970-08-26 SE SE1160070A patent/SE385242B/xx unknown
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001038170A1 (en) * | 1999-11-23 | 2001-05-31 | Technanogy, Llc | Single-stage-to-orbit rocket |
| WO2001038711A1 (en) * | 1999-11-23 | 2001-05-31 | Technanogy, Llc | End-burning rocket motor |
| RU2327052C2 (ru) * | 2006-07-26 | 2008-06-20 | Федеральное государственное унитарное предприятие "Федеральный центр двойных технологий "Союз" (ФГУП "ФЦДТ "Союз") | Способ газодинамической стабилизации давления в камере модельного двигателя с зарядами твердого ракетного топлива с высокой чувствительностью скорости горения от давления |
| RU2376490C1 (ru) * | 2008-06-11 | 2009-12-20 | Федеральное государственное унитарное предприятие "Федеральный центр двойных технологий "Союз" (ФГУП "ФЦДТ" "Союз") | Способ безынерционного определения предела минимального давления устойчивости рабочего процесса трду |
| CN111268066A (zh) * | 2020-02-27 | 2020-06-12 | 北京凌天智能装备集团股份有限公司 | 一种多功能气动抛投器 |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2064803A5 (https=) | 1971-07-23 |
| DE1943529C2 (de) | 1972-04-06 |
| BE755381A (fr) | 1971-02-01 |
| DE1943529B1 (de) | 1971-08-26 |
| SE385242B (sv) | 1976-06-14 |
| NO128365B (https=) | 1973-11-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Shidlovskii | Principles of pyrotechnics | |
| GB1216823A (en) | Solid fuel rocket engine | |
| GB1266266A (https=) | ||
| GB1171705A (en) | Improvements in or relating to Solid Fuel Rocket Propulsion Units | |
| US3646597A (en) | Variable thrust propulsion engine | |
| GB1258116A (https=) | ||
| AU465415B2 (en) | Improvements in or relating to solid propellant charges for orin rocket motors | |
| GB1133704A (en) | Preparation of nitroalkyladamantanes | |
| JPS55107039A (en) | Rocket motor | |
| GB1372324A (en) | Fuse powder composition and fuse containing the same | |
| GB1390161A (en) | Solid fuel rocket engine | |
| GB1126068A (en) | Improvements in or relating to propellant grains | |
| GB1201186A (en) | Improvements in or relating to solid rocket fuels | |
| GB1109284A (en) | Improvements in or relating to frontal burner propellent charges for rockets | |
| GB1222643A (en) | Improvements in or relating to rocket propulsion units | |
| NO158272C (no) | Artilleriprosjektil med oeket rekkevidde. | |
| SORKIN | Gas dynamics and thermodynamics of solid- propellant rockets(Soviet book on gas thermodynamics of solid propellant rocket engines covering combustion products equilibrium in nozzle and chamber, engine design, etc) | |
| US3607471A (en) | Solid composite propellants with salts of ferrocene monosulfonic acid as burning rate modifiers | |
| GB835560A (en) | Improvements in or relating to progressive charges of colloidal powder | |
| GB924690A (en) | Improved pyrotechnic device | |
| PFOERTNER | Influence of grain size on the combustion speed of solid ammonium perchlorate propellants(Influence of grain size and pressure on combustion velocity of solid ammonium perchlorate propellants) | |
| GB1323593A (en) | Launcher for missiles | |
| GB1014847A (en) | Improvements in or relating to spin-stabilised rocket projectiles | |
| JPS5612036A (en) | End face combustion type rocket motor | |
| FLETCHER et al. | A theoretical study of combustion and quenching of solid propellant rocket motors during depressurization(Conservation equations coupled with mass balance equation to produce method of computing transient burning rates in solid propellant motors) |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |