in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion

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CPC
F05D2220/80

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FMECHANICAL ENGINEERING LIGHTING HEATING WEAPONS BLASTING ENGINES OR PUMPS F05Engines, pumps F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS F05D2220/00Application

Current Industry

F05D2220/80in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion

Industries

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Patents Grantslast 30 patents

Information Patent Grant
Aircraft power plant with detonation combustion tube
- Patent number 12,203,429
- Issue date Jan 21, 2025
- Pratt & Whitney Canada Corp.
- Etienne Plamondon
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Non-axisymmetric heat shield, a nozzle defined at least partially b...
- Patent number 12,163,491
- Issue date Dec 10, 2024
- Thomas Ryan McCullough
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Annular aerospike nozzle with widely-spaced thrust chambers, engine...
- Patent number 12,152,553
- Issue date Nov 26, 2024
- Thomas Ryan McCullough
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Oxidation resistant bond coat layers, processes for coating article...
- Patent number 12,146,224
- Issue date Nov 19, 2024
- RTX Corporation
- Xia Tang
- C23 - COATING METALLIC MATERIAL COATING MATERIAL WITH METALLIC MATERIAL CHEMI...
Information Patent Grant
Supersonic aircraft and method of reducing sonic booms and jet noise
- Patent number 12,110,841
- Issue date Oct 8, 2024
- Japan Aerospace Exploration Agency
- Junichi Akatsuka
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Additively manufactured rocket fuel grains and competitive simulati...
- Patent number 12,104,558
- Issue date Oct 1, 2024
- X-Bow Launch Systems Inc.
- Chelsey Hargather
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Gas turbine operation
- Patent number 12,098,684
- Issue date Sep 24, 2024
- Rolls-Royce PLC
- Peter Swann
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Casing integrated fluid distribution system
- Patent number 12,044,409
- Issue date Jul 23, 2024
- RTX Corporation
- Lawrence A. Binek
- B22 - CASTING POWDER METALLURGY
Information Patent Grant
Supersonic air inlet of an aircraft propelling assembly comprising...
- Patent number 12,037,940
- Issue date Jul 16, 2024
- SAFRAN NACELLES
- Jean-Philippe Joret
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Supersonic speed attenuator of an air intake of an aircraft propuls...
- Patent number 12,037,941
- Issue date Jul 16, 2024
- SAFRAN NACELLES
- Jean-Philippe Joret
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Methods and systems for generating power and thermal management hav...
- Patent number 12,031,477
- Issue date Jul 9, 2024
- The Boeing Company
- Michael F. Stoia
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Jet engine
- Patent number 12,012,897
- Issue date Jun 18, 2024
- Mitsubishi Heavy Industries, Ltd.
- Shotaro Nako
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Ramjet propulsion method
- Patent number 11,976,612
- Issue date May 7, 2024
- Mark Bovankovich
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Staged combustion liquid rocket engine cycle with the turbopump uni...
- Patent number 11,970,996
- Issue date Apr 30, 2024
- Special Aerospace Services, LLC
- Timothy Bulk
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Supersonic aircraft turbofan engine
- Patent number 11,884,414
- Issue date Jan 30, 2024
- Rolls-Royce PLC
- Robert J Corin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Modulating internal ballistics in a 3D-printed rocket motor and an...
- Patent number 11,852,101
- Issue date Dec 26, 2023
- X-Bow Launch Systems Inc.
- Jason Hundley
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Liquid rocket engine booster engine with combustion gas fuel source
- Patent number 11,846,251
- Issue date Dec 19, 2023
- Firefly Aerospace Inc.
- Anatoli Alimpievich Borissov
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Segmented augmented turbine assembly
- Patent number 11,773,736
- Issue date Oct 3, 2023
- ORGANOWORLD INC.
- Frederick Churchill
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Staged combustion liquid rocket engine cycle with the turbopump uni...
- Patent number 11,708,804
- Issue date Jul 25, 2023
- Special Aerospace Services, LLC
- Timothy Bulk
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Multiple chamber rotating detonation combustor
- Patent number 11,674,476
- Issue date Jun 13, 2023
- General Electric Company
- Steven Clayton Vise
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Two-dimensional supersonic nozzle thrust vectoring using staggered...
- Patent number 11,614,050
- Issue date Mar 28, 2023
- The Regents of the University of California
- Carlos F. Montes
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine operation
- Patent number 11,591,973
- Issue date Feb 28, 2023
- Rolls-Royce PLC
- Peter Swann
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable supersonic engine inlet
- Patent number 11,591,962
- Issue date Feb 28, 2023
- The Boeing Company
- Richard K. Scharnhorst
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Attitude control and thrust boosting system and method for space la...
- Patent number 11,554,882
- Issue date Jan 17, 2023
- AVIO S.P.A
- Roberto Rosati
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method of reducing low energy flow in an isolator of a flight vehic...
- Patent number 11,473,500
- Issue date Oct 18, 2022
- Raytheon Company
- Nicholas P. Cicchini
- F42 - AMMUNITION BLASTING
Information Patent Grant
Oxidation resistant bond coat layers, processes for coating article...
- Patent number 11,459,650
- Issue date Oct 4, 2022
- Raytheon Technologies Corporation
- Xia Tang
- C23 - COATING METALLIC MATERIAL COATING MATERIAL WITH METALLIC MATERIAL CHEMI...
Information Patent Grant
Propelling nozzle for a turbofan engine on a supersonic aircraft
- Patent number 11,448,162
- Issue date Sep 20, 2022
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag Todorovic
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Engine nacelle for a gas turbine engine
- Patent number 11,428,123
- Issue date Aug 30, 2022
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Marco Rose
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Propulsion element including a catalyzing reactor
- Patent number 11,420,179
- Issue date Aug 23, 2022
- Nederlandse Organisatie voor toegepast-natuurwetenschappelijk onderzoek TNO
- Laurens Daniël Van Vliet
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Supersonic aircraft propulsion installation
- Patent number 11,383,848
- Issue date Jul 12, 2022
- Rolls-Royce PLC
- Stephen J Bradbrook
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED BASE HEAT SHIELD
- Publication number 20250052212
- Publication date Feb 13, 2025
- STOKE Space Technologies, Inc.
- Thomas Ryan McCullough
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE OPERATION
- Publication number 20240384689
- Publication date Nov 21, 2024
- Rolls-Royce plc
- Peter SWANN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHODS AND SYSTEMS FOR GENERATING POWER AND THERMAL MANAGEMENT HAV...
- Publication number 20240328348
- Publication date Oct 3, 2024
- The Boeing Company
- Michael F. Stoia
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
RAMJET PROPULSION METHOD
- Publication number 20240301844
- Publication date Sep 12, 2024
- Mark BOVANKOVICH
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
A NON-AXISYMMETRIC HEAT SHIELD, A NOZZLE DEFINED AT LEAST PARTIALLY...
- Publication number 20240208676
- Publication date Jun 27, 2024
- STOKE Space Technologies, Inc.
- Thomas Ryan McCullough
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
AIRCRAFT POWER PLANT WITH DETONATION COMBUSTION TUBE
- Publication number 20240200510
- Publication date Jun 20, 2024
- Pratt & Whitney Canada Corp.
- Etienne PLAMONDON
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOJET ENGINE REAR PORTION HAVING AN AUGMENTED A9/A8 NOZZLE AREA...
- Publication number 20240141852
- Publication date May 2, 2024
- SAFRAN AIRCRAFT ENGINES
- Thierry KOHN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MODULATING INTERNAL BALLISTICS IN A 3D-PRINTED ROCKET MOTOR AND AN...
- Publication number 20240117782
- Publication date Apr 11, 2024
- X-Bow Launch Systems Inc.
- Jason Hundley
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
SUPERSONIC AIR INLET OF AN AIRCRAFT PROPELLING ASSEMBLY COMPRISING...
- Publication number 20240018902
- Publication date Jan 18, 2024
- SAFRAN NACELLES
- Jean-Philippe Joret
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SUPERSONIC SPEED ATTENUATOR OF AN AIR INTAKE OF AN AIRCRAFT PROPULS...
- Publication number 20240018903
- Publication date Jan 18, 2024
- SAFRAN NACELLES
- Jean-Philippe Joret
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE OPERATION
- Publication number 20230323824
- Publication date Oct 12, 2023
- Rolls-Royce plc
- Peter SWANN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE SUPERSONIC ENGINE INLET
- Publication number 20230069791
- Publication date Mar 2, 2023
- The Boeing Company
- Richard K. Scharnhorst
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SEGMENTED AUGMENTED TURBINE ASSEMBLY
- Publication number 20220389824
- Publication date Dec 8, 2022
- ORGANOWORLD INC.
- Frederick CHURCHILL
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
RAMJET PROPULSION METHOD
- Publication number 20220372932
- Publication date Nov 24, 2022
- MARK BOVANKOVICH
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOC...
- Publication number 20220325678
- Publication date Oct 13, 2022
- BOOM TECHNOLOGY, INC.
- Vinod G. Mengle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ATTENUATORS FOR COMBUSTION NOISE IN DUAL MODE RAMJETS AND SCRAMJETS
- Publication number 20220282688
- Publication date Sep 8, 2022
- Raytheon Company
- Adam A. Trebs
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEMS AND METHODS FOR EXPANDING AN OPERATING SPEED RANGE OF A HIG...
- Publication number 20220195962
- Publication date Jun 23, 2022
- The Boeing Company
- Richard S. Dyer
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ENGINE NACELLE FOR A GAS TURBINE ENGINE
- Publication number 20210348525
- Publication date Nov 11, 2021
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Marco ROSE
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
PRECURSOR COMPOSITIONS FOR AN INSULATION AND INSULATED ROCKET MOTORS
- Publication number 20210079873
- Publication date Mar 18, 2021
- Northrop Grumman Innovation Systems, Inc.
- Himansu M. Gajiwala
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
PROPULSION SYSTEM FOR AN AIRCRAFT AND METHOD OF MANUFACTURING A PRO...
- Publication number 20210025352
- Publication date Jan 28, 2021
- GULFSTREAM AEROSPACE CORPORATION
- Donald Freund
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT
- Publication number 20200332741
- Publication date Oct 22, 2020
- ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Predrag TODOROVIC
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
IN-SITU SOLID ROCKET MOTOR PROPELLANT GRAIN AGING USING GAS
- Publication number 20200333224
- Publication date Oct 22, 2020
- GOODRICH CORPORATION
- Joshua David Carter
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
HYPERSONIC SUPERCONDUCTING COMBUSTION RAM ACCELERATED MAGNETOHYDROD...
- Publication number 20200284224
- Publication date Sep 10, 2020
- HyperSpace Propulsion, Inc.
- Richard H. Lugg
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
PROPULSION ELEMENT INCLUDING A CATALYZING REACTOR
- Publication number 20200164333
- Publication date May 28, 2020
- NEDERLANDSE ORGANISATIE VOOR TOEGEPAST-NATUURWETENSCHAPPELIJK ONDERZOEK TNO
- Laurens Daniël VAN VLIET
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
AFTERBURNER SYSTEM
- Publication number 20200116359
- Publication date Apr 16, 2020
- Rolls-Royce plc
- John R. WHURR
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION SYSTEM FOR AN AIRCRAFT, A NOZZLE FOR USE WITH THE PROPUL...
- Publication number 20200088132
- Publication date Mar 19, 2020
- GULFSTREAM AEROSPACE CORPORATION
- Timothy R. Conners
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
INTEGRAL VARIABLE PERFORMANCE PROPELLANT GRAIN
- Publication number 20200040849
- Publication date Feb 6, 2020
- GOODRICH CORPORATION
- Paul Parinas
- C06 - EXPLOSIVES MATCHES
Information Patent Application
SUPERSONIC AIRCRAFT TURBOFAN ENGINE
- Publication number 20200023986
- Publication date Jan 23, 2020
- Rolls-Royce plc
- Robert J. CORIN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
RAMJET PROPULSION METHOD
- Publication number 20200025150
- Publication date Jan 23, 2020
- MARK BOVANKOVICH
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SUPERSONIC AIRCRAFT PROPULSION INSTALLATION
- Publication number 20200017226
- Publication date Jan 16, 2020
- Rolls-Royce plc
- Stephen J BRADBROOK
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion

Industry

Parent Industries

Current Industry

Patents Grantslast 30 patents

Aircraft power plant with detonation combustion tube

Non-axisymmetric heat shield, a nozzle defined at least partially b...

Annular aerospike nozzle with widely-spaced thrust chambers, engine...

Oxidation resistant bond coat layers, processes for coating article...

Supersonic aircraft and method of reducing sonic booms and jet noise

Additively manufactured rocket fuel grains and competitive simulati...

Gas turbine operation

Casing integrated fluid distribution system

Supersonic air inlet of an aircraft propelling assembly comprising...

Supersonic speed attenuator of an air intake of an aircraft propuls...

Methods and systems for generating power and thermal management hav...

Jet engine

Ramjet propulsion method

Staged combustion liquid rocket engine cycle with the turbopump uni...

Supersonic aircraft turbofan engine

Modulating internal ballistics in a 3D-printed rocket motor and an...

Liquid rocket engine booster engine with combustion gas fuel source

Segmented augmented turbine assembly

Staged combustion liquid rocket engine cycle with the turbopump uni...

Multiple chamber rotating detonation combustor

Two-dimensional supersonic nozzle thrust vectoring using staggered...

Gas turbine operation

Variable supersonic engine inlet

Attitude control and thrust boosting system and method for space la...

Method of reducing low energy flow in an isolator of a flight vehic...

Oxidation resistant bond coat layers, processes for coating article...

Propelling nozzle for a turbofan engine on a supersonic aircraft

Engine nacelle for a gas turbine engine

Propulsion element including a catalyzing reactor

Supersonic aircraft propulsion installation

Patents Applicationslast 30 patents

ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED BASE HEAT SHIELD

GAS TURBINE OPERATION

METHODS AND SYSTEMS FOR GENERATING POWER AND THERMAL MANAGEMENT HAV...

RAMJET PROPULSION METHOD

A NON-AXISYMMETRIC HEAT SHIELD, A NOZZLE DEFINED AT LEAST PARTIALLY...

AIRCRAFT POWER PLANT WITH DETONATION COMBUSTION TUBE

TURBOJET ENGINE REAR PORTION HAVING AN AUGMENTED A9/A8 NOZZLE AREA...

MODULATING INTERNAL BALLISTICS IN A 3D-PRINTED ROCKET MOTOR AND AN...

SUPERSONIC AIR INLET OF AN AIRCRAFT PROPELLING ASSEMBLY COMPRISING...

SUPERSONIC SPEED ATTENUATOR OF AN AIR INTAKE OF AN AIRCRAFT PROPULS...

GAS TURBINE OPERATION

VARIABLE SUPERSONIC ENGINE INLET

SEGMENTED AUGMENTED TURBINE ASSEMBLY

RAMJET PROPULSION METHOD

LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOC...

ATTENUATORS FOR COMBUSTION NOISE IN DUAL MODE RAMJETS AND SCRAMJETS

SYSTEMS AND METHODS FOR EXPANDING AN OPERATING SPEED RANGE OF A HIG...

ENGINE NACELLE FOR A GAS TURBINE ENGINE

PRECURSOR COMPOSITIONS FOR AN INSULATION AND INSULATED ROCKET MOTORS

PROPULSION SYSTEM FOR AN AIRCRAFT AND METHOD OF MANUFACTURING A PRO...

THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT

IN-SITU SOLID ROCKET MOTOR PROPELLANT GRAIN AGING USING GAS

HYPERSONIC SUPERCONDUCTING COMBUSTION RAM ACCELERATED MAGNETOHYDROD...

PROPULSION ELEMENT INCLUDING A CATALYZING REACTOR

AFTERBURNER SYSTEM

PROPULSION SYSTEM FOR AN AIRCRAFT, A NOZZLE FOR USE WITH THE PROPUL...

INTEGRAL VARIABLE PERFORMANCE PROPELLANT GRAIN

SUPERSONIC AIRCRAFT TURBOFAN ENGINE

RAMJET PROPULSION METHOD

SUPERSONIC AIRCRAFT PROPULSION INSTALLATION