GB1313898A - Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unit - Google Patents
Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unitInfo
- Publication number
- GB1313898A GB1313898A GB3318870A GB3318870A GB1313898A GB 1313898 A GB1313898 A GB 1313898A GB 3318870 A GB3318870 A GB 3318870A GB 3318870 A GB3318870 A GB 3318870A GB 1313898 A GB1313898 A GB 1313898A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propulsion unit
- exhaust nozzle
- rocket propulsion
- reducing
- propellant
- 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
- 239000002245 particle Substances 0.000 abstract 4
- 239000003380 propellant Substances 0.000 abstract 2
- 239000006185 dispersion Substances 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 239000004449 solid propellant Substances 0.000 abstract 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
- C06D3/00—Generation of smoke or mist (chemical part)
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Botany (AREA)
- Pest Control & Pesticides (AREA)
- Plant Pathology (AREA)
- Organic Chemistry (AREA)
- Nozzles (AREA)
- Testing Of Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR6923403A FR2052048A5 (enrdf_load_stackoverflow) | 1969-07-09 | 1969-07-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1313898A true GB1313898A (en) | 1973-04-18 |
Family
ID=9037224
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3318870A Expired GB1313898A (en) | 1969-07-09 | 1970-07-08 | Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unit |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2052048A5 (enrdf_load_stackoverflow) |
GB (1) | GB1313898A (enrdf_load_stackoverflow) |
-
1969
- 1969-07-09 FR FR6923403A patent/FR2052048A5/fr not_active Expired
-
1970
- 1970-07-08 GB GB3318870A patent/GB1313898A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2052048A5 (enrdf_load_stackoverflow) | 1971-04-09 |
DE2034187A1 (de) | 1971-01-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4726279A (en) | Wake stabilized supersonic combustion ram cannon | |
GB1428411A (en) | Solid fuel rocket motors | |
GB590177A (en) | Improvements in or relating to projectiles of the rocket type | |
GB1532988A (en) | Solid fuel rocket motors | |
GB1216823A (en) | Solid fuel rocket engine | |
GB1321588A (en) | Spinstabilised rocket-propelled projectile | |
ES2013469A6 (es) | Propulsor sin tobera del tipo de alargamiento reducido. | |
GB1313898A (en) | Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unit | |
GB1468814A (en) | Rocket propulsion motors | |
GB1148431A (en) | Improvements in or relating to rocket projectiles | |
GB1205167A (en) | Improvements in or relating to armour-piercing shells | |
GB1245707A (en) | Solid propellant rocket engine | |
GB1278021A (en) | Improvements in or relating to projectiles | |
US2377247A (en) | Method and means for direct propulsion of aircraft or the like | |
GB961001A (en) | Improvements in propulsion units having a plurality of reaction propulsion nozzles | |
US3345822A (en) | Burning rate control of solid propellants | |
Yungster et al. | A numerical study of the ram accelerator concept in the superdetonative velocity range | |
GB714747A (en) | Improvements in projectiles containing an explosive in the form of a hollow charge | |
GB1222501A (en) | Tubular-shaped launcher for projectiles, in particular fr guided missiles | |
GB855591A (en) | Arrangement of rocket drive mechanisms on flying objects | |
GB824759A (en) | Improvements in or relating to supersonic barrel-fired projectiles carrying propulsion units | |
GB1450408A (en) | Method of reducing disturbance in the exhaust from a recoilless launcher | |
FR2448636A1 (fr) | Propulseur perfectionne pour roquettes et autres engins autopropulses | |
GB861433A (en) | Improvements relating to rocket motors | |
GB905550A (en) | Propellent charge |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |