DE2148319B2 - Fire-extinguishing rocket - has flap-out wall parts on load-carrying section to rotate engine section after unloading in mid-air - Google Patents

Fire-extinguishing rocket - has flap-out wall parts on load-carrying section to rotate engine section after unloading in mid-air

Info

Publication number
DE2148319B2
DE2148319B2 DE19712148319 DE2148319A DE2148319B2 DE 2148319 B2 DE2148319 B2 DE 2148319B2 DE 19712148319 DE19712148319 DE 19712148319 DE 2148319 A DE2148319 A DE 2148319A DE 2148319 B2 DE2148319 B2 DE 2148319B2
Authority
DE
Germany
Prior art keywords
rocket
wall parts
load
engine part
fire
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.)
Granted
Application number
DE19712148319
Other languages
German (de)
Other versions
DE2148319A1 (en
DE2148319C3 (en
Inventor
Beantragt Teilnichtnennung
Peter 6000 Frankfurt Aufischer
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.)
Honeywell GmbH
Original Assignee
Honeywell GmbH
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 Honeywell GmbH filed Critical Honeywell GmbH
Priority to DE19712148319 priority Critical patent/DE2148319C3/en
Priority claimed from DE19712148319 external-priority patent/DE2148319C3/en
Publication of DE2148319A1 publication Critical patent/DE2148319A1/en
Publication of DE2148319B2 publication Critical patent/DE2148319B2/en
Application granted granted Critical
Publication of DE2148319C3 publication Critical patent/DE2148319C3/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting

Abstract

Fire-extinguishing rocket consists of an engine part and a disintegratable load-carrying head whose outer wall consists of individual separate wall parts which extend parallel to the rocket axis and have their rear ends joined to the engine part, to flap out. The front parts of the wall parts are held together by a ring which can be disintegrated using a time fuze. Preferably the wall parts are locked in the flapped-out state by latches, and are inclined or curved to cause automatic rotation of the engine part when flapped out. The engine part is thus braked and brought to earth without causing damage, after the extinguishant load has been ejected. Typically the rocket is used for aircraft fins, the extinguishant beind discharged when the rocket is at the peak of its trajectory over the aircraft.
DE19712148319 1971-09-28 Extinguishing rocket Expired DE2148319C3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19712148319 DE2148319C3 (en) 1971-09-28 Extinguishing rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19712148319 DE2148319C3 (en) 1971-09-28 Extinguishing rocket

Publications (3)

Publication Number Publication Date
DE2148319A1 DE2148319A1 (en) 1973-04-05
DE2148319B2 true DE2148319B2 (en) 1975-04-10
DE2148319C3 DE2148319C3 (en) 1976-08-19

Family

ID=

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19915840A1 (en) * 1999-04-08 2000-10-12 Anton Neumeir Method and device for extinguishing forest fires from the air
CN102878870A (en) * 2012-10-24 2013-01-16 晋西工业集团有限责任公司 Extinguishment shrapnel type rocket bomb
CN102921125A (en) * 2011-08-10 2013-02-13 辽宁宇能伟业科技发展有限公司 Direct emission type remote fire extinguishing bomb
CN105890467A (en) * 2016-06-07 2016-08-24 张正泉 Detonation-free firefighting bomb

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19915840A1 (en) * 1999-04-08 2000-10-12 Anton Neumeir Method and device for extinguishing forest fires from the air
CN102921125A (en) * 2011-08-10 2013-02-13 辽宁宇能伟业科技发展有限公司 Direct emission type remote fire extinguishing bomb
CN102921125B (en) * 2011-08-10 2014-12-10 辽宁宇能伟业科技发展有限公司 Direct emission type remote fire extinguishing bomb
CN102878870A (en) * 2012-10-24 2013-01-16 晋西工业集团有限责任公司 Extinguishment shrapnel type rocket bomb
CN105890467A (en) * 2016-06-07 2016-08-24 张正泉 Detonation-free firefighting bomb

Also Published As

Publication number Publication date
DE2148319A1 (en) 1973-04-05

Similar Documents

Publication Publication Date Title
GB1329489A (en) Assembly comprising a self-propelled projectile and its case
GB376216A (en) Improvements in bladed projectiles
ES199586U (en) A toy. (Machine-translation by Google Translate, not legally binding)
ES355023A1 (en) Projectile having a useful charge which must be released at a point on the projectile trajectory
US3292302A (en) Multistage model rocket
GB1279102A (en) Improvements in or relating to assemblable missiles
GB983566A (en) Improvements in flying targets
GB1213505A (en) Missile with brake flaps
DE2148319B2 (en) Fire-extinguishing rocket - has flap-out wall parts on load-carrying section to rotate engine section after unloading in mid-air
GB1344786A (en) Pyrotechnic devices
GB851460A (en) Improvements relating to the hollow-charge warheads of projectiles
GB846069A (en) Improvements in and relating to a fin arrangement for projectiles
FR2071271A5 (en) Parachute anti-tank mine - with braking surfaces
GB1285290A (en) Doll having adjustable hair
US2485870A (en) Rocket target
GB993839A (en) Toy projectile which converts to space platform during flight
US3092027A (en) Rocket-propelled vehicle with propulsion assistant
GB1419930A (en) Container-launcher tube for rockets
GB1085045A (en) A projectile or aerial bomb
GB855591A (en) Arrangement of rocket drive mechanisms on flying objects
AVVENIRE et al. Apollo 14 mission report. Supplement 5: Descent propulsion system final flight evaluation(Performance of Apollo 14 lunar module descent propulsion system)
USD196403S (en) Outboard motor, or similar article
US2342793A (en) Aerial mine
GB1319805A (en) Arrangement comprising a jet-propelled missile and launching rockets therefor
FR2012230A1 (en) Lightweight practice round and firing - device

Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977