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Volumn , Issue , 2005, Pages

Cryogenic propulsion with zero boil-off storage applied to outer planetary exploration

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE COOLING; CRYOCOOLERS; CRYOGENIC PROPULSION; CRYOGENIC STORAGE; CRYOGENIC SYSTEM; DELTA-V; DRY MASS; EARTH RETURN VEHICLES; EFFECTIVE BLACKBODY TEMPERATURE; FIELD OF VIEWS; HYDROGEN PROPELLANT; INTERPLANETARY CRUISE; LIQUID OXYGEN; MARS SAMPLE RETURN; MECHANICALLY PUMPED; PLANETARY BODIES; PLANETARY EXPLORATION; POTENTIAL APPLICATIONS; PROPELLANT TANK; RADIATION COOLING; SAMPLE RETURN; SPACECRAFT CONFIGURATIONS; SUN SHADES; THERMAL ANALYSIS; UNMANNED EXPLORATIONS; ZERO BOIL OFFS;

EID: 77957845779     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (21)

References (11)
  • 3
    • 69249152425 scopus 로고    scopus 로고
    • Dunn, S., Coats, D., and Nickerson, G., TDK97, Two-Dimensional Kinetics (TDK) Nozzle Performance Computer Program, User's Manual, Software & Engineering Associates, Inc., NAS8-39048, Carson City, NV, January 1998.
    • Dunn, S., Coats, D., and Nickerson, G., TDK97, "Two-Dimensional Kinetics (TDK) Nozzle Performance Computer Program, User's Manual", Software & Engineering Associates, Inc., NAS8-39048, Carson City, NV, January 1998.
  • 5
    • 69249104027 scopus 로고    scopus 로고
    • Low Thrust Chemical Propulsion Pump Technology
    • NASA CR-165210
    • "Low Thrust Chemical Propulsion Pump Technology", NASA CR-165210
  • 7
    • 4143120914 scopus 로고
    • Shuttle Compatible Cryogenic Liquid Storage and Supply Systems
    • AIAA-81-1509, Colorado Springs, CO, July 27-29, AIAA 16 p
    • R. Eberhardt, et al, Shuttle Compatible Cryogenic Liquid Storage and Supply Systems, AIAA-81-1509, SAE, and ASME, Joint Propulsion Conference, 17th, Colorado Springs, CO, July 27-29, 1981, AIAA 16 p.
    • (1981) SAE, and ASME, Joint Propulsion Conference, 17th
    • Eberhardt, R.1
  • 8
    • 69249133641 scopus 로고
    • Evaluation of Propellant Tank Insulation Concepts for Low-Thrust Chemical Propulsion Systems
    • T. Kramer, E. Brogren and B. Siegel, "Evaluation of Propellant Tank Insulation Concepts for Low-Thrust Chemical Propulsion Systems", NASA CR-168320, Boeing Aerospace, 1984
    • (1984) NASA CR-168320, Boeing Aerospace
    • Kramer, T.1    Brogren, E.2    Siegel, B.3
  • 9
    • 2942589188 scopus 로고    scopus 로고
    • R. Ross, Estimation of thermal conduction loads for structural supports of cryogenic spacecraft assemblies, Cryogenics, v 44, n 6-8, June/August, 2004, 2003 Space Cryogenics Workshop, p 421-424
    • R. Ross, Estimation of thermal conduction loads for structural supports of cryogenic spacecraft assemblies, Cryogenics, v 44, n 6-8, June/August, 2004, 2003 Space Cryogenics Workshop, p 421-424
  • 10
    • 0024129536 scopus 로고    scopus 로고
    • I. Spradley & R. Parmley, Design and Test of a Modified Passive Orbital Disconnect Strut (PODS-IV), Adv. Cryo. Engin. 33 (Plenum, New York, 1988) p. 935.
    • I. Spradley & R. Parmley, Design and Test of a Modified Passive Orbital Disconnect Strut (PODS-IV), Adv. Cryo. Engin. 33 (Plenum, New York, 1988) p. 935.
  • 11
    • 69249100323 scopus 로고    scopus 로고
    • R. Parmley, S. Katz, & I. Spradley, Test and Evaluate Passive Orbital Disconnect Struts (PODS-III), NASA CR 177368, August 1985
    • R. Parmley, S. Katz, & I. Spradley, "Test and Evaluate Passive Orbital Disconnect Struts (PODS-III)", NASA CR 177368, August 1985


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.