liquid rocket engine.pdf

8/18/2019 Liquid rocket engine.pdf

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FOREWORD

NASA experience has indicated a need for uniform criteria for the design of space vehicles.

Accordingly, criteria are being developed in the following areas of technology:

Environment

Structures

Guidance and Control

Chemical Propulsion

Individual components of this work will be issued as separate monographs as soon as they

are completed. This document, part of the series on Chemical Propulsion, is one such

monograph. A list of all monographs issued prior to this one can be found on the final pages

of this document.

These monographs are to be regarded as guides to design and not as NASA requirements,

except as may be specified in formal project specifications. It is expected, however, that

these documents, revised as experience may indicate to be desirable, eventually will provide

uniform design practices for NASA space vehicles.

This monograph, Turbopump Systems for Liquid Rocket Engines, was prepared under

the direction of Howard W. Douglass, Chief, Design Criteria Office, Lewis Research Center;

project management was by Harold W. Schmidt and M. Murray Bailey. The monograph was

written by A. J. Sobin and W. R_ Bissell, Rocketdyne Division, Rockwell International

Corporation and was edited by Russell B. Keller, Jr. of Lewis. To assure technical accuracy

of this document, scientists and engineers throughout the technical community participated

in interviews, consultations, and critical review of the text. In particular, W. W. Heath of

Aerojet Liquid Rocket Company; H. M. Gibson of Pratt & Whitney Aircraft Division,


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15. Stenning, A. H.: Design of Turbines for High-Energy-Fuel, Low-Power-Output Applications. Report

79, Dynamic Anal. and Control Lab., Mass. Inst. Tech., September 1953.

16.

Balje, O.E.: A Study on Design Criteria and Matching of Turbomachines: Part A- Similarity

Relations and Design Criteria of Turbines. J. Eng. Power, Trans. ASME, Series A, vol. 84, 1962, pp.

83-102.

17. Wong, G. S.; and Wagner, W. R.: Thermodynamic Improvements in Liquid Hydrogen

Turbopumps- Second Interim Report. R-7585, Rocketdyne Div., North American Aviation, Inc.,

July 1967.

18. Huzel, D. K.; and Huang, D. W.: Design of Liquid Propellant Rocket Engines. Second ed., NASA

SP-125, 1971.

19.

20.

Dinges, R. A.: Mark 19 Final Report. TDR-3117-3011, Rocketdyne Div., North American Aviation,

Inc., unpublished, August 1963.

MacGregor, C. A.; and Csomor, A.: Rotating and Positive Displacement Pumps for Low-Thrust

Rocket Engines. NASA CR-72965, Rocketdyne Div., Rockwell International Corp., February 1974.

21. Hoshide, R. K.; and Nielson, C. E.: Study of Blade Clearance Effects on Centrifugal Pumps - Final

Report. NASA CR-120815, R-8806, Rocketdyne Div., North American Rockwell Corp., November

1972.

22.

Gelder, T. F.; Ruggeri, R. S.; and Moore, R. D.: Cavitation Similarity Considerations Based on

Measured Pressure and Temperature Depressions in Cavitated Regions of Freon-114. NASA TN

D-3509, July 1966.

23. Bissell, W. R.; Wong, G. S.; and Winstead, T. W.: Analysis of Two-Phase Flow in LH2 Pumps for

O2/H

Rocket Engines. J. Spacecraft Rockets, vol. 7, no. 6, June 1970, pp. 707-713.


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28.

29.

30.

31.

32.

33.

34.

35.

q

Anon.: Final Program Progress Report for Product Engineering, Task I, Turbomachinery (U).

R-5652-4P, Rocketdyne Div., North American Aviation, Inc., May 1965. (Confidential)

Lieblein, S.; Schwenk, J. C.; and Broderick, R. L.: Diffusion Factor for Estimating Losses and

Limiting Blade Loadings in Axial-Flow-Compressor Blade Elements. NACA RM-E53D01, 1953.

Anon.: Advanced Engine Design Study, Bell (AEB). PWA Report FR-2488 Pratt & Whitney Aircraft

Div., United Aircraft Corp., July 1967.

Anon.: H-1 Engine System Transfer Functions for Support of S-IVB Vehicle Longitudinal Stability

(Pogo). R-6813, Rocketdyne Div., North American Aviation, Inc., December 1966.

Anon.: Engine System Transfer Functions for Support of S-V Vehicle Longitudinal Stability (Pogoa

Analysis Program. R-6929, Rocketdyne Div., North American Aviation, Inc., March 1967.

Anon.: Investigation of 17 Hz Closed Loop Instability on S-II Stage of Saturn V. R-7970,

Rocketdyne Div., North American Rockwell Corp., August 1969.

Anon.: Prevention of Coupled Structure- Propulsion Instability (Pogo). Space Vehicle Design

Criteria Monograph, NASA SP-8055, October 1970.

Wieseneck, H. C.: RSS-8314-1, Space Shuttle Main Engine, Phase B, Engine System Performance

Model Program. R-8892P (Enclosure 1), Rocketdyne Div., North American Rockwell Corp., April

1971.

Mood, A.F2 Introduction to the Theory of Statistics. McGraw-Hill Book Co. (New York), 1950.

Wong, G. S.; Macgregor, C. A.; and Hoshide, R.K.: Suppression of Cavitation and Nonstable Flow in

Throttled Turbopumps. J. Spacecraft Rockets, vol. 2, no. 1, Jam-Feb. 1965, pp. 73-80.


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NASA SPACE VEHICLE DESIGN CRITERIA

MONOGRAPHS ISSUED TO DATE

ENVIRONMENT

SP-8005

SP-8010

SP-8011

SP-8013

SP-8017

SP-8020

SP-8021

SP-8023

SP-8037

SP-8038

SP-8049

SP-8067

Solar Electromagnetic Radiation, Revised May 1971

Models of Mars Atmosphere (1967), May 1968

Models of Venus Atmosphere (1972), Revised September 1972

Meteoroid Environment Model-1969 (Near Earth to Lunar Surface),

March 1969

Magnetic Fields-Earth and Extraterrestrial, March 1969

Mars Surface Models (1968), May 1969

Models of Earth's Atmosphere (90 to 2500 km), Revised March 1973

Lunar Surface Models, May 1969

Assessment and Control of Spacecraft Magnetic Fields, September 1970

Meteoroid Environment Model-1970 (Interplanetary and Planetary),

October 1970

The Earth's Ionosphere, March 1971

Earth Albedo and Emitted Radiation, July 1971


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STRUCTURES

SP-8001

SP-8002

SP-8003

SP-8004

SP-8006

SP-8007

SP-8008

SP-8009

SP-8012

SP-8014

SP-8019

SP-8022

SP-8029

SP-8030

SP-8031

BuffetingDuringAtmosphericscent,Revisedovember970

Flight-LoadsMeasurementsuringLaunchandExit, December9_4

Flutter,Buzz,andDivergence,uly1964

PanelFlutter,Revisedune1972

LocalSteadyAerodynamicoadsDuringLaunchandExit,May1965

BucklingofThin-WalledircularCylinders,Revisedugust1968

PrelaunchroundWindLoads,November965

PropellantloshLoads,August1968

NaturalVibrationModalAnalysis,September968

EntryThermalProtection,ugust1968

BucklingofThin-Walledruncatedones,September968

Stagingoads,February1969

AerodynamicndRocket-ExhausteatingDuringLaunchandAscent

May1969

TransientoadsFromThrustExcitation,February1969

SloshSuppression,ay1969


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SP-8050

SP-8053

SP-8054

SP-8055

SP-8056

SP-8057

SP-8060

SP-8061

SP-8062

SP-8063

SP-8066

SP-8068

SP-8072

SP-8077

SP-8079

StructuralVibrationPrediction,une1970

NuclearandSpaceRadiationEffectsonMaterials,une1970

SpaceRadiationProtection,une1970

PreventionfCoupledStructure-PropulsionnstabilityPogo),October

1970

FlightSeparationechanisms,ctober1970

StructuralDesignCriteriaApplicableoaSpaceShuttle,RevisedMarch

1972

Compartmententing,November970

InteractionwithUmbilicalsndLaunchStand,August1970

EntryGasdynamiceating,anuary1971

Lubrication,Friction,andWear.June971

Deployableerodynamicecelerationystems,une1971

BucklingStrengthof Structurallates,une1971

AcousticLoadsGeneratedythePropulsionystem,une1971

TransportationndHandlingoads,September971

StructuralnteractionwithControlSystems,ovember971


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SP-8016

SP-8018

SP-8024

SP-8026

SP-8027

SP-8028

SP-8033

SP-8034

SP-8036

SP-8047

SP-8058

SP-8059

SP-8065

SP-8070

SP-8071

Effectsof StructuralFlexibilityonSpacecraftontrolSystems,pril

1969

Spacecraftagneticorques,March1969

Spacecraftravitationalorques,May1969

SpacecrafttarTrackers,uly1970

SpacecraftadiationTorques,October1969

EntryVehicleControl,November969

SpacecraftarthHorizonSensors,ecember969

SpacecraftassExpulsionTorques,December969

Effectsof StructuralFlexibilityon LaunchVehicleControlSystems,

February1970

SpacecraftunSensors,une1970

Spacecrafterodynamicorques,anuary1971

SpacecraftAttitude ControlDuringThrustingManeuvers,ebruary

1971

TubularSpacecraftoomsExtendible,eelStored),February971

SpaceborneigitalComputerSystems,arch1971

Passiveravity-GradientibrationDampers,ebruary971


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CHEMICALPROPULSION

SP-8087

SP-8109

SP-8052

SP-8110

SP-8081

SP-8048

SP-8101

SP-8100

SP-8088

SP-8094

SP-8097

SP-8090

SP-8080

SP-8064

LiquidRocketEngineFluid-Cooledombustionhambers,pril 1972

LiquidRocketEngineCentrifugalFlowTurbopumps,ecember-973

LiquidRocketEngineTurbopumpnducers,May1971

LiquidRocketEngineTurbines,anuary1974

LiquidPropellantGasGenerators,arch1972

LiquidRocketEngineTurbopumpearings,arch1971

LiquidRocketEfigineTurbopumpShaftsandCouplings,eptember

1972

LiquidRocketEngineTurbopumpGears,March1974

LiquidRocketMetalTanksandTankComponents,ay1974

LiquidRocketValveComponents,ugust1973

LiquidRocketValveAssemblies,ovember973

LiquidRocketActuatorsandOperators,ay1973

LiquidRocketPressureegulators,eliefValves,CheckValves,Burst

Disks,andExplosivealves,March1973

SolidPropellantelectionndCharacterization,une1971


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