GB698390A - Improvements in rocket motors - Google Patents
Improvements in rocket motorsInfo
- Publication number
- GB698390A GB698390A GB7103/52A GB710352A GB698390A GB 698390 A GB698390 A GB 698390A GB 7103/52 A GB7103/52 A GB 7103/52A GB 710352 A GB710352 A GB 710352A GB 698390 A GB698390 A GB 698390A
- Authority
- GB
- United Kingdom
- Prior art keywords
- holder
- charges
- casing
- plates
- rocket
- 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
- 230000001133 acceleration Effects 0.000 abstract 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
- F02K9/36—Propellant charge supports
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
- Automatic Assembly (AREA)
- Testing Of Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE244651 | 1951-03-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB698390A true GB698390A (en) | 1953-10-14 |
Family
ID=38465733
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7103/52A Expired GB698390A (en) | 1951-03-21 | 1952-03-19 | Improvements in rocket motors |
Country Status (6)
Country | Link |
---|---|
BE (1) | BE510123A (de) |
CH (1) | CH299839A (de) |
ES (1) | ES202752A1 (de) |
FR (1) | FR1052581A (de) |
GB (1) | GB698390A (de) |
NL (1) | NL85039C (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015151062A1 (en) * | 2014-04-02 | 2015-10-08 | Avio S.P.A. | Solid propellant rocket motor |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4523524A (en) * | 1983-01-31 | 1985-06-18 | The United States Of America As Represented By The Secretary Of The Army | Low cost antitank rocket motor structure |
US5267513A (en) * | 1992-10-02 | 1993-12-07 | The United States Of America As Represented By The Secretary Of The Navy | Detonation through solid-state explosion fiber bundle |
-
0
- NL NL85039D patent/NL85039C/xx active
- BE BE510123D patent/BE510123A/xx unknown
-
1952
- 1952-03-19 GB GB7103/52A patent/GB698390A/en not_active Expired
- 1952-03-19 CH CH299839D patent/CH299839A/de unknown
- 1952-03-19 FR FR1052581D patent/FR1052581A/fr not_active Expired
- 1952-03-21 ES ES0202752A patent/ES202752A1/es not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015151062A1 (en) * | 2014-04-02 | 2015-10-08 | Avio S.P.A. | Solid propellant rocket motor |
US10359005B2 (en) | 2014-04-02 | 2019-07-23 | Avio S.P.A. | Solid propellant rocket motor |
Also Published As
Publication number | Publication date |
---|---|
FR1052581A (fr) | 1954-01-26 |
NL85039C (de) | |
BE510123A (de) | |
CH299839A (de) | 1954-06-30 |
ES202752A1 (es) | 1952-07-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SE389392B (sv) | Ammunitionskassett for transport och avfyrning av raketprojektiler. | |
GB698390A (en) | Improvements in rocket motors | |
GB933847A (en) | Improvements in propulsion units for rockets | |
GB720483A (en) | Powder-charge jet motors and the applications thereof | |
IT1114817B (it) | Regolatore centrifugo del numero di giri per motori endotermici ad iniezione | |
NO140206C (no) | Radial perkusjonsanordning for skytevaapen som anvender hylseloes ammunisjon med omkretstenning | |
IT7928168A0 (it) | Polvere per carica propellente pluribasica. | |
CH465967A (fr) | Moteur-fusée à charge propulsive solide | |
FR1301320A (fr) | Support éjectable de la charge propulsive pour projectile se chargeant par la bouche de l'engin de tir | |
IT989638B (it) | Tubo contenitore lanciatore per razzi | |
GB746206A (en) | Improvements relating to rocket motors | |
ALBRECHT et al. | Charge buildup on solid rockets as flame burst mechanism | |
DK112497B (da) | Ved rotation stabiliseret hulladningsraketprojektil. | |
GORDON et al. | Midcourse guidance for mariner mars 1964(Earth-based midcourse guidance for Mariner Mars 1964 space probe, using small rocket engine to obtain desired trajectory correction) | |
SHINNAR et al. | Research on mechanism of ignition of solid rocket propellants | |
IT7968473A0 (it) | Carica pirotecnica a combustione frontale particolarmente per missili e razzi | |
FR1435429A (fr) | Charge propulsive bipartite à combustion frontale et à combustible solide pour fusées | |
GB886539A (en) | Improvements relating to rocket propelled projectiles | |
FOSTER et al. | Smokeless propellants for rocket propulsion and gas generators(Cool burning smokeless propellants for gas generator applications and low signature missiles evaluated against criteria) | |
ALDER et al. | Structural-to-propellant weight ratio reduction for improved solid propellant rocket engine performance | |
BARRERE et al. | Theoretical study of bipropellant rockets employing solid grains with unequal burning rates | |
SEMENOV | Approach of two points on a circular orbit(Laws for two points closing in circular orbit in gravitational field) | |
LOFDAHL et al. | Problems and future needs associated with recording data from static firings of solid propellant motors(Transducers role in problems associated with accurate and precise measurements during static firing tests of solid propellant motors) | |
TINNAN | Discussion of the development of a winged recoverable rocket-powered launch system capable of orbiting saturn-class payloads | |
URMAN | Replacement of SR-4990 by barium styphnate in the MK 24 actuator(Barium styphnate replacement for discontinued SR-4990 smokeless powder as propellant base charge in MK 24 actuator) |