You signed in with another tab or window. Reload to refresh your session.You signed out in another tab or window. Reload to refresh your session.You switched accounts on another tab or window. Reload to refresh your session.Dismiss alert
I need to learn the structure for engine thrust profiles and adjust the water-injection pre-cooler modifications to relative values based on DARPA's projected outcomes. How could this be appropriately balanced? The Rascal is a two-stage to orbit, so I'm projecting it should flameout around 28-30km and hit about mach 3.2/3.3?
The text was updated successfully, but these errors were encountered:
I need to learn the structure for engine thrust profiles and adjust the water-injection pre-cooler modifications to relative values based on DARPA's projected outcomes. How could this be appropriately balanced? The Rascal is a two-stage to orbit, so I'm projecting it should flameout around 28-30km and hit about mach 3.2/3.3?
The text was updated successfully, but these errors were encountered: