Mars environmental survey probe aerobrake preliminary design study

Tauber, Michael E.; Henline, William D.; Chargin, M.; Papadopoulos, Periklis; Chen, Y.; Yang, Lily; Hamm, K.

doi:10.2514/3.25549

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Cited by 17 publications

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“…The heat measurements are described in the open literature [3,4]. The thermographic phosphorus [5] and temperature sensitive paint [6] techniques are used in heat measurements.…”

Section: Nomenclaturementioning

confidence: 99%

Investigation of Slender Bodies at Hypersonic Mach Numbers

Saiprakash¹,

Senthilkumar

Sunil

et al. 2021

Fluid Dyn

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Tests were carried in a shock tunnel to determine the heating rate and the wall pressure on a test model flying at hypersonic velocity. The experiments were performed at Mach M = 6.5 and a total enthalpy of 1.2 MJ/kg. Helium was used as the driver gas and air as the driven gas. The effective test time during the tunnel testing was 3.5 ms. The vacuum sputtered gages were used to evaluate the heating rate on the test model. The evaluated heating rate agrees well with numerical simulation. The experimentally measured pressure also agrees with computational fluid dynamics

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“…The heat measurements are described in the open literature [3,4]. The thermographic phosphorus [5] and temperature sensitive paint [6] techniques are used in heat measurements.…”

Section: Nomenclaturementioning

confidence: 99%