ITRM940462A0 - "dispositivo riduttore di spinta per motori a getto" - Google Patents

"dispositivo riduttore di spinta per motori a getto"

Info

Publication number
ITRM940462A0
ITRM940462A0 ITRM940462A ITRM940462A ITRM940462A0 IT RM940462 A0 ITRM940462 A0 IT RM940462A0 IT RM940462 A ITRM940462 A IT RM940462A IT RM940462 A ITRM940462 A IT RM940462A IT RM940462 A0 ITRM940462 A0 IT RM940462A0
Authority
IT
Italy
Prior art keywords
reducing device
jet engines
thrust reducing
thrust
engines
Prior art date
Application number
ITRM940462A
Other languages
English (en)
Inventor
Rainer Schoffl
Original Assignee
Dynamit Nobel Ag
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
Application filed by Dynamit Nobel Ag filed Critical Dynamit Nobel Ag
Publication of ITRM940462A0 publication Critical patent/ITRM940462A0/it
Publication of ITRM940462A1 publication Critical patent/ITRM940462A1/it
Application granted granted Critical
Publication of IT1272330B publication Critical patent/IT1272330B/it

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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/90—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using deflectors
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/92—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control incorporating means for reversing or terminating thrust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Details Of Aerials (AREA)
ITRM940462A 1993-07-16 1994-07-15 "dispositivo riduttore di spinta per motori a getto" IT1272330B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4323918A DE4323918A1 (de) 1993-07-16 1993-07-16 Einrichtung zur Schubreduzierung von Strahltriebwerken

Publications (3)

Publication Number Publication Date
ITRM940462A0 true ITRM940462A0 (it) 1994-07-15
ITRM940462A1 ITRM940462A1 (it) 1996-01-15
IT1272330B IT1272330B (it) 1997-06-16

Family

ID=6493008

Family Applications (1)

Application Number Title Priority Date Filing Date
ITRM940462A IT1272330B (it) 1993-07-16 1994-07-15 "dispositivo riduttore di spinta per motori a getto"

Country Status (3)

Country Link
DE (1) DE4323918A1 (it)
IT (1) IT1272330B (it)
NO (1) NO942640L (it)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116658332B (zh) * 2023-05-10 2026-01-30 航天科工火箭技术有限公司 一种可回收火箭返回段发动机伺服负载力矩降低装置

Also Published As

Publication number Publication date
IT1272330B (it) 1997-06-16
NO942640D0 (no) 1994-07-14
ITRM940462A1 (it) 1996-01-15
NO942640L (no) 1995-01-17
DE4323918A1 (de) 1995-01-19

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Legal Events

Date Code Title Description
0001 Granted