Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
AU499677B2 - Rocket exhaust plenum flow control apparatus - Google Patents
[go: Go Back, main page]

AU499677B2 - Rocket exhaust plenum flow control apparatus - Google Patents

Rocket exhaust plenum flow control apparatus

Info

Publication number
AU499677B2
AU499677B2 AU26197/77A AU2619777A AU499677B2 AU 499677 B2 AU499677 B2 AU 499677B2 AU 26197/77 A AU26197/77 A AU 26197/77A AU 2619777 A AU2619777 A AU 2619777A AU 499677 B2 AU499677 B2 AU 499677B2
Authority
AU
Australia
Prior art keywords
control apparatus
flow control
exhaust plenum
rocket exhaust
plenum flow
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
Application number
AU26197/77A
Other versions
AU2619777A (en
Inventor
Et Piosik
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hughes Missile Systems Co
Original Assignee
General Dynamics Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority to GB2479577A priority Critical patent/GB1540803A/en
Application filed by General Dynamics Corp filed Critical General Dynamics Corp
Priority to AU26197/77A priority patent/AU499677B2/en
Priority to NL7707074A priority patent/NL165286C/en
Priority to BE1008258A priority patent/BE856528A/en
Priority to DE19772731060 priority patent/DE2731060C2/en
Priority to FR7720918A priority patent/FR2396950A1/en
Publication of AU2619777A publication Critical patent/AU2619777A/en
Application granted granted Critical
Publication of AU499677B2 publication Critical patent/AU499677B2/en
Assigned to HUGHES MISSILE SYSTEMS COMPANY reassignment HUGHES MISSILE SYSTEMS COMPANY Alteration of Name(s) in Register under S187 Assignors: GENERAL DYNAMICS CORPORATION
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/0413Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G1/00Arrangements of guns or missile launchers; Vessels characterised thereby

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Exhaust Gas After Treatment (AREA)
AU26197/77A 1977-06-14 1977-06-17 Rocket exhaust plenum flow control apparatus Expired AU499677B2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB2479577A GB1540803A (en) 1977-06-14 1977-06-14 Rocket exhaust plenum flow control apparatus
AU26197/77A AU499677B2 (en) 1977-06-14 1977-06-17 Rocket exhaust plenum flow control apparatus
NL7707074A NL165286C (en) 1977-06-14 1977-06-24 DEVICE FOR THE SAFE DISSIPATION OF EXHAUST GASES, FOR EXAMPLE, MISSILES.
BE1008258A BE856528A (en) 1977-06-14 1977-07-06 ROCKET EXHAUST MANIFOLD FLOW CONTROL DEVICE
DE19772731060 DE2731060C2 (en) 1977-06-14 1977-07-07 Missile launcher
FR7720918A FR2396950A1 (en) 1977-06-14 1977-07-07 ROCKET EXHAUST MANIFOLD FLOW CONTROL DEVICE

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
GB2479577A GB1540803A (en) 1977-06-14 1977-06-14 Rocket exhaust plenum flow control apparatus
AU26197/77A AU499677B2 (en) 1977-06-14 1977-06-17 Rocket exhaust plenum flow control apparatus
NL7707074A NL165286C (en) 1977-06-14 1977-06-24 DEVICE FOR THE SAFE DISSIPATION OF EXHAUST GASES, FOR EXAMPLE, MISSILES.
BE856528 1977-07-06
BE1008258A BE856528A (en) 1977-06-14 1977-07-06 ROCKET EXHAUST MANIFOLD FLOW CONTROL DEVICE
DE19772731060 DE2731060C2 (en) 1977-06-14 1977-07-07 Missile launcher
FR7720918A FR2396950A1 (en) 1977-06-14 1977-07-07 ROCKET EXHAUST MANIFOLD FLOW CONTROL DEVICE

Publications (2)

Publication Number Publication Date
AU2619777A AU2619777A (en) 1978-12-21
AU499677B2 true AU499677B2 (en) 1979-04-26

Family

ID=27560520

Family Applications (1)

Application Number Title Priority Date Filing Date
AU26197/77A Expired AU499677B2 (en) 1977-06-14 1977-06-17 Rocket exhaust plenum flow control apparatus

Country Status (6)

Country Link
AU (1) AU499677B2 (en)
BE (1) BE856528A (en)
DE (1) DE2731060C2 (en)
FR (1) FR2396950A1 (en)
GB (1) GB1540803A (en)
NL (1) NL165286C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU636264B2 (en) * 1991-05-13 1993-04-22 Raytheon Company Multi-missile canister gas management system

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2143895B (en) * 1983-07-23 1987-01-21 Bernard James Hargreaves Pyramidal reed valves for two-stroke engines
FR2620808B1 (en) * 1987-09-17 1990-01-12 France Etat Armement REAR LID FOR MISSILE CONTAINER

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445423A (en) * 1946-03-06 1948-07-20 United Shoe Machinery Corp Safety container for rockets
US2965116A (en) * 1955-12-06 1960-12-20 Opw Corp Emergency shut-off valve for remote pump pedestal units

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU636264B2 (en) * 1991-05-13 1993-04-22 Raytheon Company Multi-missile canister gas management system

Also Published As

Publication number Publication date
FR2396950A1 (en) 1979-02-02
GB1540803A (en) 1979-02-14
DE2731060C2 (en) 1982-04-01
NL165286B (en) 1980-10-15
NL165286C (en) 1980-10-15
AU2619777A (en) 1978-12-21
DE2731060A1 (en) 1979-01-11
BE856528A (en) 1978-01-06
FR2396950B1 (en) 1983-04-08
NL7707074A (en) 1978-12-28

Similar Documents

Publication Publication Date Title
AU511655B2 (en) Controlled airflow oven
AU535208B2 (en) Variable area exhaust nozzle
GB2018970B (en) Combustion control apparatus
JPS5331016A (en) Control apparatus for turbine supercharger
AU511342B2 (en) Air/fuel ratio control
AU515327B2 (en) Flow control baffles
GB2042770B (en) Exhaust gas recirculation rate control device
AU527589B2 (en) Control system for gas operated apparatus
GB2061567B (en) Gas turbine control system
AU522051B2 (en) Air duct outlet
AU521828B2 (en) Engine control
AU530576B2 (en) An exhaust gas recirculation control system
AU520797B2 (en) Air control valve
GB2010405B (en) Gas turbine control systems
ZA773454B (en) Intake control apparatus
JPS5444116A (en) Fuel control apparatus
AU499677B2 (en) Rocket exhaust plenum flow control apparatus
JPS5425523A (en) Gas valve control apparatus
AU494774B2 (en) Intake control apparatus
AU491273B2 (en) An exhaust gas recirculation control system
AU2599477A (en) Intake control apparatus
AU494590B2 (en) An exhaust gas recirculation control system
AU494334B2 (en) An exhaust gas recirculation control system
AU495817B2 (en) Improved exhaust gas recirculation control system
AU502229B2 (en) Engine control system