Publication Date:
2019-07-13
Description:
In an earlier report thermal stresses, simulating those expected on a Mars Lander, dislodged approximately 0.01% of an aerosol deposited surface burden, as did a landing shock of 8-10 G deceleration. This work confirms earlier results and demonstrates that release rate is not dependent on surface burden.
Keywords:
BIOSCIENCES
Type:
NASA-CR-139621
,
QR-1
Format:
application/pdf