GB1473749A - Monopropellant thruster with superheater - Google Patents
Monopropellant thruster with superheaterInfo
- Publication number
- GB1473749A GB1473749A GB1990075A GB1990075A GB1473749A GB 1473749 A GB1473749 A GB 1473749A GB 1990075 A GB1990075 A GB 1990075A GB 1990075 A GB1990075 A GB 1990075A GB 1473749 A GB1473749 A GB 1473749A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- super
- heater
- disposed
- hydrazine
- 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
- OAKJQQAXSVQMHS-UHFFFAOYSA-N Hydrazine Chemical compound NN OAKJQQAXSVQMHS-UHFFFAOYSA-N 0.000 abstract 8
- 238000000354 decomposition reaction Methods 0.000 abstract 5
- 230000004888 barrier function Effects 0.000 abstract 1
- 238000007599 discharging Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
- 238000010438 heat treatment Methods 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
- F02K9/42—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
- F02K9/68—Decomposition chambers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/411—Electric propulsion
- B64G1/415—Arcjets or resistojets
-
- C—CHEMISTRY; METALLURGY
- C06—EXPLOSIVES; MATCHES
- C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
- C06D5/00—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
- C06D5/04—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by auto-decomposition of single substances
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Organic Chemistry (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US54319575A | 1975-01-22 | 1975-01-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1473749A true GB1473749A (en) | 1977-05-18 |
Family
ID=24166979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1990075A Expired GB1473749A (en) | 1975-01-22 | 1975-05-12 | Monopropellant thruster with superheater |
Country Status (7)
| Country | Link |
|---|---|
| JP (1) | JPS5950865B2 (enrdf_load_stackoverflow) |
| CA (1) | CA999749A (enrdf_load_stackoverflow) |
| DE (1) | DE2535520C3 (enrdf_load_stackoverflow) |
| FR (1) | FR2298699A1 (enrdf_load_stackoverflow) |
| GB (1) | GB1473749A (enrdf_load_stackoverflow) |
| IT (1) | IT1045168B (enrdf_load_stackoverflow) |
| NL (1) | NL174815C (enrdf_load_stackoverflow) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3209470A1 (de) * | 1981-03-19 | 1982-09-30 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland, London | Elektrothermisches reaktionstriebwerk |
| DE3128735A1 (de) * | 1981-07-21 | 1983-02-10 | Erno-Raumfahrttechnik Gmbh, 2800 Bremen | Triebwerk, insbesondere fuer raumflugkoerper |
| DE3141354A1 (de) * | 1981-10-17 | 1983-04-28 | Erno-Raumfahrttechnik Gmbh, 2800 Bremen | "triebwerk, insbesondere steuertriebwerk fuer raumflugkoerper" |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1534601A (en) * | 1976-07-23 | 1978-12-06 | Secr Defence | Electrothermal gas thrusters |
| GB1557590A (en) * | 1976-10-25 | 1979-12-12 | Secr Defence | Gas thrusters |
| DE2854276A1 (de) * | 1977-12-14 | 1979-06-28 | Hawker Siddeley Dynamics Ltd | Einrichtung mit zufuehrung fluessigen brennstoffs zum erzeugen einer heissen stroemung |
| US4305247A (en) * | 1979-06-18 | 1981-12-15 | Hughes Aircraft Company | Electrothermally augmented hydrazine thruster |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3016693A (en) * | 1960-09-23 | 1962-01-16 | John R Jack | Electro-thermal rocket |
| US3210927A (en) * | 1963-10-01 | 1965-10-12 | Paul F Brinich | Electro-thermal rockets having improved heat exchangers |
| US3603093A (en) * | 1970-03-06 | 1971-09-07 | Nasa | Heated porous plug microthrustor |
-
1975
- 1975-05-12 GB GB1990075A patent/GB1473749A/en not_active Expired
- 1975-05-16 NL NLAANVRAGE7505797,A patent/NL174815C/xx not_active IP Right Cessation
- 1975-05-16 CA CA227,125A patent/CA999749A/en not_active Expired
- 1975-06-12 JP JP50071415A patent/JPS5950865B2/ja not_active Expired
- 1975-06-16 IT IT83638/75A patent/IT1045168B/it active
- 1975-06-16 FR FR7518763A patent/FR2298699A1/fr active Granted
- 1975-08-08 DE DE2535520A patent/DE2535520C3/de not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3209470A1 (de) * | 1981-03-19 | 1982-09-30 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland, London | Elektrothermisches reaktionstriebwerk |
| DE3128735A1 (de) * | 1981-07-21 | 1983-02-10 | Erno-Raumfahrttechnik Gmbh, 2800 Bremen | Triebwerk, insbesondere fuer raumflugkoerper |
| US4470258A (en) * | 1981-07-21 | 1984-09-11 | Erno Raumfahrttechnik Gmbh | Thruster for space vehicles |
| DE3141354A1 (de) * | 1981-10-17 | 1983-04-28 | Erno-Raumfahrttechnik Gmbh, 2800 Bremen | "triebwerk, insbesondere steuertriebwerk fuer raumflugkoerper" |
Also Published As
| Publication number | Publication date |
|---|---|
| NL7505797A (nl) | 1976-07-26 |
| DE2535520C3 (de) | 1978-12-07 |
| NL174815C (nl) | 1984-08-16 |
| DE2535520B2 (enrdf_load_stackoverflow) | 1978-04-13 |
| FR2298699B1 (enrdf_load_stackoverflow) | 1978-02-24 |
| IT1045168B (it) | 1980-05-10 |
| FR2298699A1 (fr) | 1976-08-20 |
| JPS5187610A (en) | 1976-07-31 |
| NL174815B (nl) | 1984-03-16 |
| CA999749A (en) | 1976-11-16 |
| JPS5950865B2 (ja) | 1984-12-11 |
| DE2535520A1 (de) | 1976-07-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4322946A (en) | Thermal thruster with superheater | |
| US5485721A (en) | Arcjet for a space flying body | |
| GB1405847A (en) | Dual thrust level monopropellant spacecraft propulsion system | |
| US3159967A (en) | Variable thrust ion engine utilizing thermally decomposable solid fuel | |
| US3982488A (en) | Flueric through bulkhead rocket motor ignitor | |
| US3151447A (en) | Igniter device | |
| US3651644A (en) | Apparatus for initiating decomposition of an exothermic propellant | |
| US5697212A (en) | Rocket propellant tank self-pressurization | |
| GB1473749A (en) | Monopropellant thruster with superheater | |
| US3392673A (en) | Consumable pyrogen igniter | |
| US4470258A (en) | Thruster for space vehicles | |
| US3263418A (en) | Detonation reaction engine | |
| GB1534601A (en) | Electrothermal gas thrusters | |
| US3371491A (en) | Thrust direction modification means | |
| US4305247A (en) | Electrothermally augmented hydrazine thruster | |
| US3533233A (en) | Hot gas generator utilizing a mono-propellant fuel | |
| US3471106A (en) | Valveless microrocket systems | |
| US3197959A (en) | Control apparatus | |
| US3013388A (en) | Gas generating apparatus | |
| US3457726A (en) | Incrementally controllable-thrust propulsion device | |
| FR2385075A1 (fr) | Missile autopropulse destine a exploser dans l'atmosphere | |
| US3231002A (en) | Pulsed chamber pressurization system | |
| US3583161A (en) | Radioisotope/electrothermal thruster | |
| US3107487A (en) | Rocket motor | |
| US3273335A (en) | Manifold ignition system for solid propellant rockets |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19920512 |