2020-09-05
3 indexed posts · All posts for this date, newest first.
@Erdayastronaut @PPathole @SpaceX Above 50% likely to make it
View post →Captured source text.
@PPathole @SpaceX This is a test engine. Flight articles are fixed with no gimbal.
View post →Captured source text.
@SpaceX Worth noting that thrust is only slightly higher with the big bell nozzle version. Larger bell is primarily for efficiency in vacuum. Aiming for 380+ sec Isp for RVac long-term. Initially likely to be ~372.
View post →Captured source text.