IT1196948B - INSULATING MASS FOR AN INSULATING LAYER ON A CHARGE OF SOLID PROPELLENT FOR ROCKETS - Google Patents
INSULATING MASS FOR AN INSULATING LAYER ON A CHARGE OF SOLID PROPELLENT FOR ROCKETSInfo
- Publication number
- IT1196948B IT1196948B IT21083/86A IT2108386A IT1196948B IT 1196948 B IT1196948 B IT 1196948B IT 21083/86 A IT21083/86 A IT 21083/86A IT 2108386 A IT2108386 A IT 2108386A IT 1196948 B IT1196948 B IT 1196948B
- Authority
- IT
- Italy
- Prior art keywords
- insulating
- rockets
- charge
- insulating layer
- mass
- Prior art date
Links
- 239000007787 solid Substances 0.000 title 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
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
- F02K9/346—Liners, e.g. inhibitors
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
- C06B45/00—Compositions or products which are defined by structure or arrangement of component of product
- C06B45/12—Compositions or products which are defined by structure or arrangement of component of product having contiguous layers or zones
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K5/00—Use of organic ingredients
- C08K5/16—Nitrogen-containing compounds
- C08K5/20—Carboxylic acid amides
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Crystallography & Structural Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Polyurethanes Or Polyureas (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19853528505 DE3528505A1 (en) | 1985-08-08 | 1985-08-08 | INSULATING DIMENSION FOR AN INSULATING LAYER ON A ROCKET SOLID FUEL SET |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| IT8621083A0 IT8621083A0 (en) | 1986-07-10 |
| IT8621083A1 IT8621083A1 (en) | 1988-01-10 |
| IT1196948B true IT1196948B (en) | 1988-11-25 |
Family
ID=6278048
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT21083/86A IT1196948B (en) | 1985-08-08 | 1986-07-10 | INSULATING MASS FOR AN INSULATING LAYER ON A CHARGE OF SOLID PROPELLENT FOR ROCKETS |
Country Status (4)
| Country | Link |
|---|---|
| DE (1) | DE3528505A1 (en) |
| FR (1) | FR2586016A1 (en) |
| GB (1) | GB2178745B (en) |
| IT (1) | IT1196948B (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3643824A1 (en) * | 1986-12-20 | 1988-06-30 | Bayern Chemie Gmbh Flugchemie | Liner layer for lining rocket combustion chambers |
| US4810729A (en) * | 1987-10-23 | 1989-03-07 | Basf Corporation | Flexible flame resistant polyurethane foams |
| DE3829958A1 (en) * | 1988-09-03 | 1990-03-08 | Bayer Ag | METHOD FOR PRODUCING POLYURETHANE FOAMS |
| JPH08231291A (en) * | 1994-12-27 | 1996-09-10 | Daicel Chem Ind Ltd | Gas generating agent composition |
| FR2745037B1 (en) * | 1996-02-20 | 1998-05-07 | Europ Propulsion | METHOD FOR PRODUCING AN INTERNAL THERMAL PROTECTION FOR A PROPELLER |
| RU2208007C2 (en) * | 2001-06-13 | 2003-07-10 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" | Inhibiting composition for solid rocket fuel charges |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1605219A (en) * | 1962-03-28 | 1973-08-31 | Solid propergols based on polyurethanes - catalysed with zinc dimercapto benzimidazolate for better mechanical and combustion properties | |
| JPS4819299B1 (en) * | 1969-12-25 | 1973-06-12 | ||
| FR2159668A5 (en) * | 1971-11-08 | 1973-06-22 | Poudres & Explosifs Ste Nale | Primers for solid propergols (butargols) - contg polyurethanes and polyepoxides |
| US4187215A (en) * | 1972-09-25 | 1980-02-05 | Aerojet-General Corporation | Polymeric isocyanate-hydroxy terminated polybutadiene compositions |
| GB2038346B (en) * | 1978-12-21 | 1983-02-16 | Secr Defence | Inhibition coating for propellant charges |
-
1985
- 1985-08-08 DE DE19853528505 patent/DE3528505A1/en active Granted
-
1986
- 1986-07-10 IT IT21083/86A patent/IT1196948B/en active
- 1986-07-22 GB GB08617884A patent/GB2178745B/en not_active Expired
- 1986-08-07 FR FR8611439A patent/FR2586016A1/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| FR2586016A1 (en) | 1987-02-13 |
| DE3528505C2 (en) | 1989-05-18 |
| IT8621083A1 (en) | 1988-01-10 |
| DE3528505A1 (en) | 1987-02-19 |
| IT8621083A0 (en) | 1986-07-10 |
| GB8617884D0 (en) | 1986-08-28 |
| GB2178745A (en) | 1987-02-18 |
| GB2178745B (en) | 1988-08-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB2164416B (en) | An active vibration isolating device | |
| IT1187824B (en) | COMBUSTION INHIBITOR COMPOSITION PARTICULARLY FOR PROPULSIVE CHARGES OF MISSILES | |
| IT1196948B (en) | INSULATING MASS FOR AN INSULATING LAYER ON A CHARGE OF SOLID PROPELLENT FOR ROCKETS | |
| TR23652A (en) | PROCEDURE FOR SELECTIVE REMOVAL OF ADHESIVE MATERIALS FROM POLIIMID SUB-LAYERS | |
| GB8610822D0 (en) | Magnetostrictive transducer | |
| GB2105443B (en) | Insulating layer for a solid-fuel rocket engine | |
| IT8467016A0 (en) | PERCUSSION DEVICE FOR IGNITION OF THE IGNITION OF AN EXPLOSIVE CHARGE | |
| GB8507596D0 (en) | Piezoelectric transducer | |
| DK161043C (en) | ROCKET LAUNCH UNIT | |
| ES551126A0 (en) | AN APPARATUS FOR PRE-ASSEMBLY OF A INJECTOR SUB-ASSEMBLY | |
| DK49186A (en) | DRIVING ORGANIZATION FOR AN ELECTROMECHANICAL VIBRATOR | |
| IT1201400B (en) | PROPULSOR COMPLEX WITH CENTRIFUGAL MASS OFFERING THRUST REACTION | |
| IT1115185B (en) | PROPULSIVE CHARGE OF AMMUNITION | |
| FR2590178B1 (en) | PERFORATOR-INJECTOR COMPRISING AN INTERNAL PERCUSSION MASS | |
| GB8802914D0 (en) | Producing insulating layer on rocket solid propellant charge | |
| IT1155601B (en) | METHOD FOR REALIZING A BASE OF AN ALTERNATIVE ENDOTHERMAL MOTOR AND BASE MADE WITH SUCH PROCEDURE | |
| GB8801575D0 (en) | Solid rocket motor propellants with reticulated structures embedded therein & method of manufacture thereof | |
| IT8423488A1 (en) | Triggering device for a propellant charge | |
| IT8521015U1 (en) | STRUCTURE OF A DEVICE FOR LAUNCHING AND DEFINING A BURIED CHARGE | |
| GB8506311D0 (en) | Explosive hardening of cast portion | |
| KR880018414U (en) | Feeding structure of piezoelectric vibrator | |
| GB2200362B (en) | Intermediate layer between solid propellant charge and insulating layer thereof | |
| IT8648058A0 (en) | COMPOSITE PROPELLANT CHARGE FOR LAUNCHING PROJECTILES | |
| IT8319664A0 (en) | CARTRIDGE STRUCTURE SUITABLE FOR IMPROVING THE POWER OF AN EXPLOSIVE CHARGE. | |
| IT1188628B (en) | TIME DELAY DEVICE OF ELECTRONIC SIGNALS |