Preliminary Analysis of the Rocket Plug Nozzle Combined Cycle (RPNCC) Propulsion System

2009 ◽  
Author(s):  
Dustin Wood
Keyword(s):  
Preliminary Analysis ◽  
Combined Cycle ◽  
Propulsion System ◽  
Plug Nozzle

scholarly journals Performance Analysis of Combined Cycle with Air Breathing Derivative Gas Turbine, Heat Recovery Steam Generator, and Steam Turbine as LNG Tanker Main Engine Propulsion System

2020 ◽  
Vol 8 (9) ◽  
pp. 726
Author(s):  
Wahyu Nirbito ◽  
Muhammad Arif Budiyanto ◽  
Robby Muliadi
Keyword(s):  
Performance Analysis ◽  
Steam Turbine ◽  
Gas Turbine ◽  
Steam Generator ◽  
Heat Recovery ◽  
Combined Cycle ◽  
Propulsion System ◽  
Heat Recovery Steam Generator ◽  
Main Engine ◽  
Ship Speed

This study explains the performance analysis of a propulsion system engine of an LNG tanker using a combined cycle whose components are gas turbine, steam turbine, and heat recovery steam generator. The researches are to determine the total resistance of an LNG tanker with a capacity of 125,000 m3 by using the Maxsurf Resistance 20 software, as well as to design the propulsion system to meet the required power from the resistance by using the Cycle-Tempo 5.0 software. The simulation results indicate a maximum power of the system of about 28,122.23 kW with a fuel consumption of about 1.173 kg/s and a system efficiency of about 48.49% in fully loaded conditions. The ship speed can reach up to 20.67 knots.

Turbo/air augmented rocket - A combined cycle propulsion system

1989 ◽  
Author(s):  
A. GANJI ◽  
M. KHADEM ◽  
S. KHANDANI
Keyword(s):  
Combined Cycle ◽  
Propulsion System

XFV-12A Propulsion System Development

1976 ◽  
Author(s):  
J. T. Delany ◽  
G. M. Jenkins
Keyword(s):  
System Design ◽  
Development Process ◽  
System Development ◽  
Full Scale ◽  
Propulsion System ◽  
Design And Development ◽  
Plug Nozzle ◽  
Design Philosophy ◽  
Thrust System ◽  
Testing And Evaluation

The XFV-12A total powered lift/thrust system being developed under contract for the U. S. Navy is described. The description includes design and development to date of the inlets, engine integration, the diverter valve with plug nozzle, the lift system augmenter supply ducting, and lift/thrust augmenter hardware. The development process description includes system design philosophy and criteria, analysis, test facilities utilized, model and full-scale testing and evaluation.

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