FR1315914A - Engine for rockets or missiles of the multi-section or multi-element type and solid fuel - Google Patents
Engine for rockets or missiles of the multi-section or multi-element type and solid fuelInfo
- Publication number
- FR1315914A FR1315914A FR881998A FR881998A FR1315914A FR 1315914 A FR1315914 A FR 1315914A FR 881998 A FR881998 A FR 881998A FR 881998 A FR881998 A FR 881998A FR 1315914 A FR1315914 A FR 1315914A
- Authority
- FR
- France
- Prior art keywords
- rockets
- missiles
- engine
- section
- solid fuel
- 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
- 235000015842 Hesperis Nutrition 0.000 title 1
- 235000012633 Iberis amara Nutrition 0.000 title 1
- 239000004449 solid propellant 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
- F02K9/343—Joints, connections, seals therefor
-
- 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
- F02K9/18—Shape or structure of solid propellant charges of the internal-burning type having a star or like shaped internal cavity
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR881998A FR1315914A (en) | 1961-03-01 | 1961-12-14 | Engine for rockets or missiles of the multi-section or multi-element type and solid fuel |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB755661A GB918936A (en) | 1961-03-01 | 1961-03-01 | Improvements in or relating to rocket motors |
FR881998A FR1315914A (en) | 1961-03-01 | 1961-12-14 | Engine for rockets or missiles of the multi-section or multi-element type and solid fuel |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1315914A true FR1315914A (en) | 1963-01-25 |
Family
ID=26193522
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR881998A Expired FR1315914A (en) | 1961-03-01 | 1961-12-14 | Engine for rockets or missiles of the multi-section or multi-element type and solid fuel |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1315914A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2461728C2 (en) * | 2010-12-03 | 2012-09-20 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" | Solid-propellant rocket engine |
WO2013019898A1 (en) * | 2011-08-01 | 2013-02-07 | The Aerospace Corporation | Systems and methods for casting hybrid rocket motor fuel grains |
US8601790B2 (en) | 2008-02-28 | 2013-12-10 | The Aerospace Corporation | Buried radial flow rapid prototyping rocket motors |
US8707676B2 (en) | 2008-02-28 | 2014-04-29 | The Aerospace Corporation | Radial flow rapid prototyping rocket motors |
US8844133B2 (en) | 2008-02-28 | 2014-09-30 | The Aerospace Corporation | Stereolithographic rocket motor manufacturing method |
US9038368B2 (en) | 2011-08-01 | 2015-05-26 | The Aerospace Corporation | Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor |
-
1961
- 1961-12-14 FR FR881998A patent/FR1315914A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8601790B2 (en) | 2008-02-28 | 2013-12-10 | The Aerospace Corporation | Buried radial flow rapid prototyping rocket motors |
US8707676B2 (en) | 2008-02-28 | 2014-04-29 | The Aerospace Corporation | Radial flow rapid prototyping rocket motors |
US8844133B2 (en) | 2008-02-28 | 2014-09-30 | The Aerospace Corporation | Stereolithographic rocket motor manufacturing method |
RU2461728C2 (en) * | 2010-12-03 | 2012-09-20 | Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" | Solid-propellant rocket engine |
WO2013019898A1 (en) * | 2011-08-01 | 2013-02-07 | The Aerospace Corporation | Systems and methods for casting hybrid rocket motor fuel grains |
US9038368B2 (en) | 2011-08-01 | 2015-05-26 | The Aerospace Corporation | Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor |
US9429104B2 (en) | 2011-08-01 | 2016-08-30 | The Aerospace Corporation | Systems and methods for casting hybrid rocket motor fuel grains |
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