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1
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11744273384
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The Surface Evolver
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K. A. Brakke. The Surface Evolver. Experimental Mathematics, 1(2):141-165, 1992.
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(1992)
Experimental Mathematics
, vol.1
, Issue.2
, pp. 141-165
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Brakke, K.A.1
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6
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85088766618
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Effects of an elliptic end-cap on the ullage bubble stability in the Gravity Probe-B satellite
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In Reno, NV, January. AIAA-96-0596
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Robert L. Bayt and Steven H. Collicott. Effects of an elliptic end-cap on the ullage bubble stability in the Gravity Probe-B satellite. In 34th AIAA Aerospace Sciences Meeting, Reno, NV, January 1996. AIAA-96-0596.
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(1996)
34th AIAA Aerospace Sciences Meeting
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Bayt, R.L.1
Collicott, S.H.2
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7
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0004489059
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Ullage bubble stability in the Gravity Probe-B helium tank
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In Indianapolis, IN, June. AIAA paper number AIAA-94-3026
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Steven H. Collicott, Robert L. Bayt, and Scott D. Courtney. Ullage bubble stability in the Gravity Probe-B helium tank. In 30th AIAA Joint Propuslion Conference, Indianapolis, IN, June 1994. AIAA paper number AIAA-94-3026.
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(1994)
30th AIAA Joint Propuslion Conference
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Collicott, S.H.1
Bayt, R.L.2
Courtney, S.D.3
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12
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85088721477
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Investigation of the wetting behavior of a vane-wall gap in propellant tanks
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In July. AIAA-2002-3986
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Y. Chen and S. H. Collicott. Investigation of the wetting behavior of a vane-wall gap in propellant tanks. In 38th AIAA Joint Propulsion Conference and Exhibit, July 2002. AIAA-2002-3986.
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(2002)
38th AIAA Joint Propulsion Conference and Exhibit
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Chen, Y.1
Collicott, S.H.2
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13
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10944225703
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Technical report, Martin Marietta, Sept. MCR-91-1346, Contract NAS3-25977
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J. Gille and T. Martin. Vented tank resupply experiment (VTRE), final technology requirements document. Technical report, Martin Marietta, Sept. 1993. MCR-91-1346, Contract NAS3-25977.
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(1993)
Vented tank resupply experiment (VTRE), final technology requirements document.
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Gille, J.1
Martin, T.2
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14
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84963860919
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Propellant management device analysis for some off-design operational scenarios
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In Los Angeles, CA, June AIAA-99-2974
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G. P. Purohit, J. R. Ellison, and D. E. Jr. Jaekle. Propellant management device analysis for some off-design operational scenarios. In 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, CA, June 1999. AIAA-99-2974.
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(1999)
35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
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Purohit, G.P.1
Ellison, J.R.2
Jaekle Jr., D.E.3
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15
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84983112842
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Convergence behavior of Surface Evolver applied to a generic propellant management device
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In Reno, NV, AIAA-99-0846, also in press at Journal of Propulsion and Power, expected June 2001
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S. H. Collicott. Convergence behavior of Surface Evolver applied to a generic propellant management device. In 37th AIAA Aerospace Sciences Meeting, Reno, NV, 1999. AIAA-99-0846, also in press at Journal of Propulsion and Power, expected June 2001.
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(1999)
37th AIAA Aerospace Sciences Meeting
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Collicott, S.H.1
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