GB1102625A - Creation of Inventions and Patents with Artificial Intelligence

GB1102625A – Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles
– Google Patents

GB1102625A – Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles
– Google Patents
Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles

Info

Publication number
GB1102625A

GB1102625A
GB44580/65A
GB4458065A
GB1102625A
GB 1102625 A
GB1102625 A
GB 1102625A
GB 44580/65 A
GB44580/65 A
GB 44580/65A
GB 4458065 A
GB4458065 A
GB 4458065A
GB 1102625 A
GB1102625 A
GB 1102625A
Authority
GB
United Kingdom
Prior art keywords
rocket
gas
nozzles
reservoir
attitude
Prior art date
1964-10-22
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
GB44580/65A
Inventor
Roger Adrien Feraud
Jean Paul Joseph Jardinier
Rue Antoine Mimerel
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.)

Safran Aircraft Engines SAS

Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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.)
1964-10-22
Filing date
1965-10-21
Publication date
1968-02-07

1965-10-21
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS
filed
Critical
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA

1968-02-07
Publication of GB1102625A
publication
Critical
patent/GB1102625A/en

Status
Expired
legal-status
Critical
Current

Links

Espacenet

Global Dossier

Discuss

235000015842
Hesperis
Nutrition

0.000
title
1

235000012633
Iberis amara
Nutrition

0.000
title
1

230000006641
stabilisation
Effects

0.000
title
1

239000007800
oxidant agent
Substances

0.000
abstract
2

230000001590
oxidative effect
Effects

0.000
abstract
2

239000003380
propellant
Substances

0.000
abstract
2

238000002485
combustion reaction
Methods

0.000
abstract
1

238000010276
construction
Methods

0.000
abstract
1

239000007788
liquid
Substances

0.000
abstract
1

230000001141
propulsive effect
Effects

0.000
abstract
1

Classifications

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F41—WEAPONS

F41G—WEAPON SIGHTS; AIMING

F41G7/00—Direction control systems for self-propelled missiles

F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data

F41G7/36—Direction control systems for self-propelled missiles based on predetermined target position data using inertial references

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

F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases

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

F42B10/02—Stabilising arrangements

F42B10/26—Stabilising arrangements using spin

F42B10/28—Stabilising arrangements using spin induced by gas action

F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles

F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING

F42—AMMUNITION; BLASTING

F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION

F42B10/60—Steering arrangements

F42B10/66—Steering by varying intensity or direction of thrust

F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Abstract

1,102,625. Controlling rocket propelled missiles. SOCIETE NATIONALE D’ETUDE ET DE CONSTRUCTION DE MOTEURS D’AVIATION. 21 Oct., 1965 [22 Oct., 1964], No. 44580/65. Heading B7G. A sounding rocket is propelled by liquid propellant and oxidant forced into a rocket motor from tanks (2, 3, Fig. 1, not shown) by gas pressure, e.g. from a gas reservoir (4). During powered flight the attitude of the rocket in pitch and yaw is controlled by propellant or oxidant forced by gas pressure through inwardly directed nozzles 10, 11 in the walls of the jet pipe 9, thus deflecting the propulsive jet. Roll control is effected by supplying gas from the reservoir (4) to tangentially directed nozzles 12 outside the rocket. During unpowered flight, roll, pitch and yaw control are all effected by externally directed nozzles supplied with gas from the reservoir, and different roll control nozzles, smaller than those for powered flight are used. The changeover to these nozzles is made either by a timer set to the duration of the powered flight, or by a pressure switch responsive to combustion chamber pressure. The attitude is controlled by gyroscopes 13 and rate gyros 15 and by an attitude reference 17, the signals from which are summed and used to control valves such as 19.

GB44580/65A
1964-10-22
1965-10-21
Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles

Expired

GB1102625A
(en)

Applications Claiming Priority (1)

Application Number
Priority Date
Filing Date
Title

FR992324A

FR1423755A
(en)

1964-10-22
1964-10-22

Stabilization device and steering sounding rockets and other vehicles

Publications (1)

Publication Number
Publication Date

GB1102625A
true

GB1102625A
(en)

1968-02-07

Family
ID=8840880
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

GB44580/65A
Expired

GB1102625A
(en)

1964-10-22
1965-10-21
Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles

Country Status (3)

Country
Link

US
(1)

US3350886A
(en)

FR
(1)

FR1423755A
(en)

GB
(1)

GB1102625A
(en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

GB1605295A
(en)

1967-12-13
1988-06-08
Secr Defence
Rocket projectiles

US3614026A
(en)

1969-04-29
1971-10-19
Us Air Force
Self-sustained attitude control system

US3747342A
(en)

1970-11-18
1973-07-24
Us Navy
Control system for flexible seal movable nozzle

US4063685A
(en)

1976-07-30
1977-12-20
The United States Of America As Represented By The Secretary Of The Army
Thrust vector control by circulation control over aerodynamic surfaces in a supersonic nozzle

US5028014A
(en)

1988-11-15
1991-07-02
Anderson Jr Carl W
Radial bleed total thrust control apparatus and method for a rocket propelled missile

US5158246A
(en)

1988-11-15
1992-10-27
Anderson Jr Carl W
Radial bleed total thrust control apparatus and method for a rocket propelled missile

US5564267A
(en)

1995-05-10
1996-10-15
Leaf-Pro, Inc.
Raking and pick-up tool

US5823478A
(en)

1995-07-17
1998-10-20
The University Of British Columbia
Pressure feed for liquid propellant

US7082750B2
(en)

2002-08-09
2006-08-01
Knight Andrew F
Pressurizer for a rocket engine

US7229029B2
(en)

2002-10-29
2007-06-12
Phisser Technologies, Inc.
Propulsion system

US6918243B2
(en)

2003-05-19
2005-07-19
The Boeing Company
Bi-propellant injector with flame-holding zone igniter

US8122703B2
(en)

2006-04-28
2012-02-28
United Technologies Corporation
Coaxial ignition assembly

US7989744B2
(en)

2008-02-01
2011-08-02
Raytheon Company
Methods and apparatus for transferring a fluid

US11313650B2
(en)

2012-03-02
2022-04-26
Northrop Grumman Systems Corporation
Methods and apparatuses for aerial interception of aerial threats

US9170070B2
(en)

2012-03-02
2015-10-27
Orbital Atk, Inc.
Methods and apparatuses for active protection from aerial threats

US9501055B2
(en)

2012-03-02
2016-11-22
Orbital Atk, Inc.
Methods and apparatuses for engagement management of aerial threats

US8975565B2
(en)

2012-07-17
2015-03-10
Raytheon Company
Integrated propulsion and attitude control system from a common pressure vessel for an interceptor

US9377279B2
(en)

2014-04-22
2016-06-28
Raytheon Company
Rocket cluster divert and attitude control system

US11346306B1
(en)

2019-01-03
2022-05-31
Ball Aerospace & Technologies Corp.
Chemical and cold gas propellant systems and methods

US11498705B1
(en)

2019-05-09
2022-11-15
Ball Aerospace & Technology Corp.
On orbit fluid propellant dispensing systems and methods

US11292617B1
(en)

2019-07-24
2022-04-05
National Technology & Egineering Solutions Of Sandia, Llc
Spin-stabilized orbital rocket guidance

CN112344807B
(en)

2020-10-27
2022-08-09
中国运载火箭技术研究院
Carrier rocket

Family Cites Families (9)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

US2671312A
(en)

1948-11-20
1954-03-09
Onera (Off Nat Aerospatiale)
Device for feeding reagents to the mixing chambers of rockets

US2943821A
(en)

1950-12-30
1960-07-05
United Aircraft Corp
Directional control means for a supersonic vehicle

US3015210A
(en)

1958-12-24
1962-01-02
Bendix Corp
Attitude control for high altitude missile

US3134225A
(en)

1960-03-02
1964-05-26
Thompson Ramo Wooldridge Inc
Thrust control system

US3115887A
(en)

1961-02-23
1963-12-31
Thompson Ramo Wooldridge Inc
Missile roll control valve system

US3213611A
(en)

1962-04-23
1965-10-26
Bendix Corp
Valve

US3170290A
(en)

1962-07-20
1965-02-23
James E Webb
Liquid rocket system

US3190069A
(en)

1963-01-28
1965-06-22
Bell Aerospace Corp
Space vehicle control system

US3230706A
(en)

1963-02-11
1966-01-25
Thompson Ramo Wooldridge Inc
Leakage detector

1964

1964-10-22
FR
FR992324A
patent/FR1423755A/en
not_active
Expired

1965

1965-10-21
GB
GB44580/65A
patent/GB1102625A/en
not_active
Expired

1965-10-21
US
US500078A
patent/US3350886A/en
not_active
Expired – Lifetime

Also Published As

Publication number
Publication date

DE1453868B2
(en)

1975-08-07

FR1423755A
(en)

1966-01-07

DE1453868A1
(en)

1969-09-18

US3350886A
(en)

1967-11-07

Contact information