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1

United States. National Aeronautics and Space Administration., ed. 1050 K Stirling space engine design. National Aeronautics and Space Administration, 1988.

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2

United States. National Aeronautics and Space Administration., ed. 1050 K Stirling space engine design. National Aeronautics and Space Administration, 1988.

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3

Center, NASA Glenn Research, and United States. National Aeronautics and Space Administration., eds. Stirling Space Engine Program. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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4

M, Meyer Claudia, and Lewis Research Center, eds. Space engine safety system. National Aeronautics and Space Administration, Lewis Research Center, 1991.

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5

Center, NASA Glenn Research, and United States. National Aeronautics and Space Administration., eds. Stirling Space Engine Program. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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6

United States. National Aeronautics and Space Administration., ed. Space Transportation Booster Engine Configuration Study. United Technologies, Pratt & Whitney, 1989.

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7

I, Masters A., and United States. National Aeronautics and Space Administration., eds. Advanced Engine Study program. National Aeronautics and Space Administration, 1993.

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8

United States. National Aeronautics and Space Administration., ed. Space Transportation Engine Program (STEP): Phase B. Rockwell International, Rocketdyne Division, 1990.

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9

Duyar, Ahmet. Identification of space shuttle main engine dynamics. National Aeronautics and Space Administration, 1989.

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10

United States. National Aeronautics and Space Administration., ed. Space Transportation Engine Program (STEP): Phase B. Rockwell International, Rocketdyne Division, 1990.

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11

George C. Marshall Space Flight Center., ed. Space shuttle main engine turbopump bearing assessment program. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.

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12

George C. Marshall Space Flight Center., ed. Space shuttle main engine turbopump bearing assessment program. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.

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13

Erickson, C. M. Orbit transfer rocket engine technology program: Final report : advanced engine study, task D.6. Rocketdyne Division of Rockwell International Corporation, 1992.

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14

T, Welch John, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Analysis of the space shuttle main engine simulation. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1993.

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15

Lyndon B. Johnson Space Center., ed. STS-59 space shuttle mission report. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1994.

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16

Lyndon B. Johnson Space Center., ed. STS-59 space shuttle mission report. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1994.

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17

Erickson, C. M. Orbit transfer rocket engine technology program: Phase II : interim report : advanced engine study, task D.4. Rocketdyne Division, Rockwell International Corporation, 1988.

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18

D, Southwick R., and United States. National Aeronautics and Space Administration., eds. Large liquid rocket engine transient performance simulation system. Pratt & Whitney, 1989.

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19

D, Southwick R., and United States. National Aeronautics and Space Administration., eds. Large liquid rocket engine transient performance simulation system. United Technologies, Pratt & Whitney ; [Washington, DC, 1989.

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20

Lyndon B. Johnson Space Center., ed. STS-62 space shuttle mission report. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1994.

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21

Lyndon B. Johnson Space Center., ed. STS-62 space shuttle mission report. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1994.

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22

Lyndon B. Johnson Space Center., ed. STS-62 space shuttle mission report. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1994.

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23

E, Roschak, and Lewis Research Center, eds. Orbit transfer rocket engine technology: 7.5K-lb thrust rocket engine preliminary design : final report. NASA-Lewis Research Center, 1993.

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24

Lyndon B. Johnson Space Center., ed. STS-80 Space Shuttle Program Mission. Lyndon B. Johnson Space Center, 1997.

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25

United States. National Aeronautics and Space Administration., ed. Space transportation booster engine thrust chamber technology: Final report. Aerojet Propulsion Division, 1993.

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26

United States. National Aeronautics and Space Administration., ed. Rocketdyne safety algorithm: Space shuttle main engine fault detection. National Aeronautics and Space Administration, 1994.

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27

United States. National Aeronautics and Space Administration., ed. Progress toward the evolution of a Stirling space engine. National Aeronautics and Space Administration, 1988.

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28

United States. National Aeronautics and Space Administration., ed. NASA, orbital transfer rocket engine technology: Advanced engine study, task D.6 final report : contract no. NAS 3-23772. National Aeronautics and Space Administration, 1992.

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29

D, Southwick R., and George C. Marshall Space Flight Center., eds. Large liquid rocket engine transient performance simulation system: Final report. United Technologies Corporation, Pratt & Whitney, Government Engine Business, 1991.

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30

L, Musgrave Jeffrey, Walker Bruce K, and United States. National Aeronautics and Space Administration., eds. On-line implementation of nonlinear parameter estimation for the space shuttle main engine. National Aeronautics and Space Administration, 1992.

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31

L, Musgrave Jeffrey, Walker Bruce K, and United States. National Aeronautics and Space Administration., eds. On-line implementation of nonlinear parameter estimation for the space shuttle main engine. National Aeronautics and Space Administration, 1992.

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32

Payne, Roger. ALS engine propellant effector system: Summary final report. Aerojet Propulsion Division, 1993.

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33

C, Rapp Douglas, and United States. National Aeronautics and Space Administration., eds. Reliability studies of Integrated modular engine system designs. National Aeronautics and Space Administration, 1993.

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34

Rauch, Jeffrey. Transient and steady-state tests of the space power research engine with resistive and motor loads. National Aeronautics and Space Administration, 1995.

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35

Rauch, Jeffrey. Transient and steady-state tests of the space power research engine with resistive and motor loads. National Aeronautics and Space Administration, 1995.

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36

Rauch, Jeffrey. Transient and steady-state tests of the space power research engine with resistive and motor loads. National Aeronautics and Space Administration, 1995.

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37

Rauch, Jeffrey. Transient and steady-state tests of the space power research engine with resistive and motor loads. National Aeronautics and Space Administration, 1995.

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38

United States. National Aeronautics and Space Administration., ed. Space Transportation Booster Engine (STBE) configuration study: Second quarterly review. National Aeronautics and Space Administration, 1986.

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39

Ahmet, Duyar, and United States. National Aeronautics and Space Administration., eds. A simplified dynamic model of the space shuttle main engine. National Aeronautics and Space Administration, 1991.

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40

W, Hawman Michael, United Technologies Research Center, and Lewis Research Center, eds. Framework for a space shuttle main engine health monitoring system. United Technologies Research Center, 1990.

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41

T, Gawrylowicz Henry, and United States. National Aeronautics and Space Administration., eds. Structural integrity and durability for space shuttle main engine and future reusable space propulsion systems. National Aeronautics and Space Administration, 1986.

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42

Lynn, E. Elizabeth. Main propulsion system test requirements for the two-engine shuttle-C. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1990.

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43

United States. National Aeronautics and Space Administration., ed. Space shuttle main engine plume plowfield model: Final report : research study. Remtech Inc., 1988.

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44

United States. National Aeronautics and Space Administration., ed. Overview of free-piston Stirling engine technology for space power application. National Aeronautics and Space Administration, 1988.

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45

United States. National Aeronautics and Space Administration., ed. Overview of free-piston Stirling engine technology for space power application. National Aeronautics and Space Administration, 1988.

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46

United States. National Aeronautics and Space Administration., ed. Overview of free-piston Stirling engine technology for space power application. National Aeronautics and Space Administration, 1988.

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47

J, Harmon T., and Lewis Research Center, eds. Orbit transfer rocket engine technology program: Final report. NASA-Lewis Research Center, 1993.

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48

United States. National Aeronautics and Space Administration., ed. Final report, space shuttle main engine structural analysis and data reduction/evaluation. Lockheed-Huntsville Engineering Center, 1989.

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49

Foley, Michael J. Space shuttle main engine structural analysis and data reduction/evaluation.: Final report. Lockheed Missiles & Space Co., Inc., Huntsville Engineering Center, 1989.

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50

Paxson, Daniel E. A model for the space shuttle main engine high pressure oxidizer turbopump shaft seal system. National Aeronautics and Space Administration, 1991.

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