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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Inc., unpublished, August 1963.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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C I
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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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