-
1
-
-
18444395479
-
A feasibility study of heat-pipe-cooled leading edges for hypersonic cruise aircraft
-
Nov.
-
Silverstein, C. C., "A Feasibility Study of Heat-Pipe-Cooled Leading Edges for Hypersonic Cruise Aircraft," NASA CR-1857, Nov. 1971.
-
(1971)
NASA CR-1857
-
-
Silverstein, C.C.1
-
2
-
-
0016057270
-
Four space shuttle wing leading edge concepts
-
Niblock, G. A., Reeder, J. C., and Huneidi, F., "Four Space Shuttle Wing Leading Edge Concepts," Journal of Spacecraft and Rockets, Vol. 11, No. 5, 1974, pp. 314-320.
-
(1974)
Journal of Spacecraft and Rockets
, vol.11
, Issue.5
, pp. 314-320
-
-
Niblock, G.A.1
Reeder, J.C.2
Huneidi, F.3
-
3
-
-
18444388777
-
Space shuttle orbiter heat pipe application
-
April
-
Alario, J. P., and Prager, R. C., "Space Shuttle Orbiter Heat Pipe Application," NASA CR-128498, April 1972.
-
(1972)
NASA CR-128498
-
-
Alario, J.P.1
Prager, R.C.2
-
4
-
-
18444401640
-
Study of structural active cooling and heat sink systems for space shuttle
-
June
-
"Study of Structural Active Cooling and Heat Sink Systems for Space Shuttle," NASA CR-123912, June 1972.
-
(1972)
NASA CR-123912
-
-
-
5
-
-
84976463971
-
Design, fabrication, testing, and delivery of shuttle heat pipe leading edge test modules
-
April
-
"Design, Fabrication, Testing, and Delivery of Shuttle Heat Pipe Leading Edge Test Modules," NASA CR-124425, April 1973.
-
(1973)
NASA CR-124425
-
-
-
6
-
-
84915055888
-
Analysis and radiant heating tests of a heat-pipe-cooled leading edge
-
Aug.
-
Camarda, C. J., "Analysis and Radiant Heating Tests of a Heat-Pipe-Cooled Leading Edge," NASA TN-D-8468, Aug. 1977.
-
(1977)
NASA TN-D-8468
-
-
Camarda, C.J.1
-
7
-
-
18444396071
-
Aerothermal tests of a heat-pipe-cooled leading edge at mach 7
-
Nov.
-
Camarda, C. J., "Aerothermal Tests of a Heat-Pipe-Cooled Leading Edge at Mach 7," NASA TP-1320, Nov. 1978.
-
(1978)
NASA TP-1320
-
-
Camarda, C.J.1
-
8
-
-
0019478067
-
Design, analysis, and tests of a shuttle-type heat-pipe-cooled leading edge
-
Camarda, C. J., and Masek, R. V., "Design, Analysis, and Tests of a Shuttle-Type Heat-Pipe-Cooled Leading Edge," Journal of Spacecraft and Rackets, Vol. 18, No. 1, 1981, pp. 71-78.
-
(1981)
Journal of Spacecraft and Rackets
, vol.18
, Issue.1
, pp. 71-78
-
-
Camarda, C.J.1
Masek, R.V.2
-
9
-
-
18444412167
-
Thermostructural applications of heat pipes
-
June
-
Peeples, M. E., Reeder, J. C., and Sontag, K. E., "Thermostructural Applications of Heat Pipes," NASA CR-159096, June 1979.
-
(1979)
NASA CR-159096
-
-
Peeples, M.E.1
Reeder, J.C.2
Sontag, K.E.3
-
10
-
-
18444397359
-
Heat pipes for wing leading edges of hypersonic vehicles
-
Jan.
-
Boman, B. L., Citrin, E. C., Garner, E. C., and Stone, J. E., "Heat Pipes for Wing Leading Edges of Hypersonic Vehicles," NASA CR-181922, Jan. 1990.
-
(1990)
NASA CR-181922
-
-
Boman, B.L.1
Citrin, E.C.2
Garner, E.C.3
Stone, J.E.4
-
11
-
-
85006932862
-
Tests on a sodium/hastelloy X wing leading edge heat pipe for hypersonic vehicles
-
June
-
Boman, B. L., and Elias, T., "Tests on a Sodium/Hastelloy X Wing Leading Edge Heat Pipe for Hypersonic Vehicles," AIAA Paper 90-1759, June 1990.
-
(1990)
AIAA Paper 90-1759
-
-
Boman, B.L.1
Elias, T.2
-
12
-
-
5244226528
-
Modeling of Startup from the frozen state
-
Grenoble, France, May
-
Colwell, G. T., Jang, J. H., and Camarda, C. J., "Modeling of Startup from the Frozen State," 6th International Heat Pipe Conf., Grenoble, France, May 1987.
-
(1987)
6th International Heat Pipe Conf.
-
-
Colwell, G.T.1
Jang, J.H.2
Camarda, C.J.3
-
13
-
-
0343496078
-
Preliminary thermal/structural analysis of a carbon-carbon/refractory-metal heat-pipe-cooled wing leading edge
-
edited by E. A. Thomton, Progress in Astronautics and Aeronautics, AIAA, Washington, DC
-
Glass, D. E., and Camarda, C. J., "Preliminary Thermal/Structural Analysis of a Carbon-Carbon/Refractory-Metal Heat-Pipe-Cooled Wing Leading Edge," Thermal Structures and Materials for High Speed Flight, edited by E. A. Thomton, Vol. 140, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1992, pp. 301-322.
-
(1992)
Thermal Structures and Materials for High Speed Flight
, vol.140
, pp. 301-322
-
-
Glass, D.E.1
Camarda, C.J.2
-
14
-
-
0027063061
-
Fabrication of carbon-carbon heat pipes for space nuclear power applications
-
San Diego, CA, Aug.
-
Rovang, R. D., Palamides, T. R., and Hunt, M. E., "Fabrication of Carbon-Carbon Heat Pipes for Space Nuclear Power Applications," 27th Intersociety Energy Conversion Engineering Conf., San Diego, CA, Aug. 1992.
-
(1992)
27th Intersociety Energy Conversion Engineering Conf.
-
-
Rovang, R.D.1
Palamides, T.R.2
Hunt, M.E.3
-
15
-
-
18444416733
-
Fabrication and testing of Mo-Re heat pipes embedded in carbon/carbon
-
March
-
Glass, D. E., Merrigan, M. A., and Sena, J. T., "Fabrication and Testing of Mo-Re Heat Pipes Embedded in Carbon/Carbon," NASA CR-1998-207642, March 1998.
-
(1998)
NASA CR-1998-207642
-
-
Glass, D.E.1
Merrigan, M.A.2
Sena, J.T.3
-
16
-
-
0343496077
-
-
U.S. Patent 5,720,339, Feb.
-
Glass, D. E., Camarda, C. J., and Merrigan, M. A., "Refractory-Composite/Heat-Pipe-Cooled Leading Edge," U.S. Patent 5,720,339, Feb. 1998.
-
(1998)
Refractory-Composite/Heat-Pipe-Cooled Leading Edge
-
-
Glass, D.E.1
Camarda, C.J.2
Merrigan, M.A.3
-
17
-
-
85088283007
-
Transient performance investigation of a space power system heat pipe
-
June
-
Merrigan, M. A., Keddy, E. S., and Sena, J. T., "Transient Performance Investigation of a Space Power System Heat Pipe," AIAA Paper 86-1273, June 1986.
-
(1986)
AIAA Paper 86-1273
-
-
Merrigan, M.A.1
Keddy, E.S.2
Sena, J.T.3
-
18
-
-
18444384985
-
Oxidation and emittance studies of coated Mo-Re
-
Oct.
-
Glass, D. E., "Oxidation and Emittance Studies of Coated Mo-Re," NASA CR-201753, Oct. 1997.
-
(1997)
NASA CR-201753
-
-
Glass, D.E.1
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