FR2515736B1 - METHOD OF MANUFACTURING A LOAD OF PROPERGOL AND PROPELLANT LOAD COMPRISING SUCH A LOAD - Google Patents
METHOD OF MANUFACTURING A LOAD OF PROPERGOL AND PROPELLANT LOAD COMPRISING SUCH A LOADInfo
- Publication number
- FR2515736B1 FR2515736B1 FR8120446A FR8120446A FR2515736B1 FR 2515736 B1 FR2515736 B1 FR 2515736B1 FR 8120446 A FR8120446 A FR 8120446A FR 8120446 A FR8120446 A FR 8120446A FR 2515736 B1 FR2515736 B1 FR 2515736B1
- Authority
- FR
- France
- Prior art keywords
- load
- propergol
- manufacturing
- propellant
- propellant load
- 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
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
- F02K9/10—Shape or structure of solid propellant charges
- F02K9/14—Shape or structure of solid propellant charges made from sheet-like materials, e.g. of carpet-roll type, of layered structure
-
- 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
- F02K9/36—Propellant charge supports
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 |
---|---|---|---|
FR8120446A FR2515736B1 (en) | 1981-10-30 | 1981-10-30 | METHOD OF MANUFACTURING A LOAD OF PROPERGOL AND PROPELLANT LOAD COMPRISING SUCH A LOAD |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8120446A FR2515736B1 (en) | 1981-10-30 | 1981-10-30 | METHOD OF MANUFACTURING A LOAD OF PROPERGOL AND PROPELLANT LOAD COMPRISING SUCH A LOAD |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2515736A1 FR2515736A1 (en) | 1983-05-06 |
FR2515736B1 true FR2515736B1 (en) | 1986-06-27 |
Family
ID=9263583
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8120446A Expired FR2515736B1 (en) | 1981-10-30 | 1981-10-30 | METHOD OF MANUFACTURING A LOAD OF PROPERGOL AND PROPELLANT LOAD COMPRISING SUCH A LOAD |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2515736B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102015106822A1 (en) * | 2015-04-30 | 2016-11-03 | Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh | Motor drive with high boost / sustain thrust ratios |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR69519E (en) * | 1956-04-03 | 1958-11-10 | Soc Tech De Rech Ind | Propellant charge for powder reaction vehicles |
US3159104A (en) * | 1959-11-02 | 1964-12-01 | Solid Fuels Corp | Laminated tape propellants |
US3664133A (en) * | 1965-06-30 | 1972-05-23 | Us Navy | Supported grain design for high acceleration rocket motors |
FR2053681A5 (en) * | 1969-07-15 | 1971-04-16 | Ramont Jacques | Solid fuel propellant |
FR2067962A5 (en) * | 1969-11-24 | 1971-08-20 | Etud Realisa Applic Tech | Rocket propellant charges |
FR2181178A6 (en) * | 1970-12-04 | 1973-11-30 | France Etat | Polyurethane resin propellant rod support - loaded with fillers and rein-forced for greater heat stability |
US4013743A (en) * | 1973-02-12 | 1977-03-22 | Rockwell International Corporation | Spiral grain solid propellant fabrication process |
FR2356116A1 (en) * | 1973-07-13 | 1978-01-20 | France Etat | IMPROVEMENTS TO HOT POWDERING GAS GENERATORS AND PROCESSES FOR THE PREPARATION OF THEIR CHARGE |
FR2283419A1 (en) * | 1974-06-27 | 1976-03-26 | Poudres & Explosifs Ste Nale | Propulsive charge with partially inhibited bands - notably for use in anti-tank rockets |
FR2299519A1 (en) * | 1975-01-31 | 1976-08-27 | Poudres & Explosifs Ste Nale | Charge of projectile propellant with combustion inhibitor - covering propellant surfaces in part and destroyed after time delay |
FR2334648A1 (en) * | 1975-12-12 | 1977-07-08 | Poudres & Explosifs Ste Nale | Pyrotechnical, lamellar charge in combustion inhibiting sleeve - is moulded flat and rolled into cylinder fitting projectile |
-
1981
- 1981-10-30 FR FR8120446A patent/FR2515736B1/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2515736A1 (en) | 1983-05-06 |
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