Flight performance of Crew Escape System during pad abort condition.

Autor: Somanath, S.1 s_somanath@vssc.gov.in, Nair, S. Unnikrishnan2, Sivamurugan, T.1, Desikan, S. L. N.1
Zdroj: Current Science (00113891). 1/10/2021, Vol. 120 Issue 1, p81-88. 8p.
Databáze: Academic Search Ultimate