Weigand et al., 2020 - Google Patents
A Solid Propellant Rocket Motor for a Sounding RocketWeigand et al., 2020
- Document ID
- 10341386714665401015
- Author
- Weigand A
- Ringeisen A
- Meyer T
- Naumann K
- Kirchhartz R
- Jung W
- Scheuerpflug F
- Publication year
- Publication venue
- AIAA Propulsion and Energy 2020 Forum
External Links
Snippet
The paper gives a brief overview on the performance and design aspects of a new Sounding Rocket Motor with the name “Red Kite®”. The German Aerospace Center (DLR) and its Mobile Rocket Base (MORABA) contracted propulsion company Bayern-Chemie GmbH to …
- 239000004449 solid propellant 0 title abstract description 6
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F02K9/97—Rocket nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F02K9/34—Casings; Combustion chambers; Liners thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- 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
- F02K9/36—Propellant charge supports
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8967046B2 (en) | Gas generators, launch tubes including gas generators and related systems and methods | |
US7762195B2 (en) | Slow cook off rocket igniter | |
US4213393A (en) | Gun projectile arranged with a base drag reducing system | |
US6619029B2 (en) | Rocket motors with insensitive munitions systems | |
US4972673A (en) | Solid rocket motor with dual interrupted thrust | |
US4573412A (en) | Plug nozzle kinetic energy penetrator rocket | |
Naumann et al. | Double-pulse solid rocket motor technology-applications and technical solutions | |
US3561362A (en) | Free punch with attached power plant | |
US2613605A (en) | Projectile | |
Weigand et al. | A Solid Propellant Rocket Motor for a Sounding Rocket | |
KR101987170B1 (en) | Ramjet Solid Fuel with Ignition Support for Gun-Propelled Ramjet Shell | |
US9169806B2 (en) | Propulsion system for flying machine, particularly for a missile | |
US4170875A (en) | Caseless rocket design | |
Dahl et al. | Demonstration of solid propellant pulse motor technologies | |
US6494035B1 (en) | Towing rocket motor assembly | |
Naumann et al. | A First Stage Solid Propellant Rocket Motor for Sounding Rockets | |
US5022306A (en) | Method of ejecting an interceptor missile from its silo | |
Jaafar et al. | Development of solid rocket propulsion system at UTM | |
US11486682B2 (en) | Integrated propulsion and warhead system for an artillery round | |
EP4354077A1 (en) | A solid fuel propelled projectile | |
US11988173B2 (en) | Multi-pulse propulsion system with passive initiation | |
Sparks et al. | Fifty years of solid propellant technical achievements at Atlantic Research Corporation | |
Zhang | Design and Analysis of the Two-Stage FGM-148 Javelin Anti-Tank Missile | |
BR102022019307A2 (en) | LONG-RANGE SUPERSONIC BALLISTIC ROCKET WITH JET STATE PROPULSION | |
Shubov | Feasibility of Rocket Artillery Systems With Reusable First Stage |