FR1592900A - - Google Patents
Info
- Publication number
- FR1592900A FR1592900A FR1592900DA FR1592900A FR 1592900 A FR1592900 A FR 1592900A FR 1592900D A FR1592900D A FR 1592900DA FR 1592900 A FR1592900 A FR 1592900A
- Authority
- FR
- France
- 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
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
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
-
- 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
- F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19671626072 DE1626072A1 (en) | 1967-11-25 | 1967-11-25 | Rocket combustion process and gas generator (combustion chamber) to carry out the process |
DE19671626071 DE1626071A1 (en) | 1967-11-25 | 1967-11-25 | Rocket combustion process and gas generator to carry out the process |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1592900A true FR1592900A (en) | 1970-05-19 |
Family
ID=25753857
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1592900D Expired FR1592900A (en) | 1967-11-25 | 1968-11-22 |
Country Status (2)
Country | Link |
---|---|
US (1) | US3555824A (en) |
FR (1) | FR1592900A (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4957242A (en) * | 1988-04-12 | 1990-09-18 | The United States Of America As Represented By The Secretary Of The Navy | Fluid mixing device having a conical inlet and a noncircular outlet |
US7503165B2 (en) * | 2004-09-29 | 2009-03-17 | Spacedev, Inc. | Hybrid propulsion system |
US7404288B2 (en) * | 2004-10-28 | 2008-07-29 | Spacedev, Inc. | High propulsion mass fraction hybrid propellant system |
US7966809B2 (en) | 2006-02-01 | 2011-06-28 | Spacedev, Inc. | Single-piece hybrid rocket motor |
US8539753B2 (en) * | 2006-06-29 | 2013-09-24 | Spacedev, Inc. | Hybrid rocket motor with annular, concentric solid fuel elements |
WO2020041675A1 (en) * | 2018-08-23 | 2020-02-27 | Rocket Crafters Propulsion Llc | Linear throttling high regression rate vortex flow field injection system within a hybrid rocket engine |
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1968
- 1968-11-22 FR FR1592900D patent/FR1592900A/fr not_active Expired
- 1968-11-22 US US778205A patent/US3555824A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US3555824A (en) | 1971-01-19 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |