Publication Date:
2019-08-26
Description:
Provide plume induced heating (radiation & convection) predictions in support of the LDSD thermal design (pre-flight SFDT-1) Predict plume induced aerodynamics in support of flight dynamics, to achieve targeted freestream conditions to test supersonic deceleration technologies (post-flight SFDT-1, pre-flight SFDT-2)
Keywords:
Aerodynamics; Spacecraft Design, Testing and Performance
Type:
M16-5363
,
International Planetary Probe Conference; Jun 13, 2016 - Jun 17, 2016; Laurel, MD; United States
Format:
application/pdf
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