erikwriter
New Member
I realize that is a very long title for this thread. I previously joined a conversation mid thread a few days ago and asked a couple questions about the Blackhawk during the inception of TF-160. I got some pretty awesome answers in response. I thought I would start a new thread and see if I could dive a little deeper.
I have been reading about the creation of TF-160 in the book, The Night Stalkers, by Durant, Hartov and Col. Johnson. In it, they discuss how there were growing pains with the Blackhawks during fast and low training missions and that some pilots and machines were lost.
I asked if some of these losses had anything to do with differences in flying a Blackhawk versus a Chinook or a Huey. Was there an adjustment period pilots experienced because of the Hawks engines, or rotor blades? Was there a difference in rotor RPM (is that a thing) or maybe the power to weight ratio that took some getting used to.
One person told me that one aspect of the Hawk that took some adjustment was the inertia of the rotor head. As a civilian I have no idea what that means. The same gentleman said the the Hawk also had more tail rotor authority. I assume that means it was more responsive and took some getting used to.
Another individual said the loss in Hawks in the beginning of TF-160 was more about the development of new, more aggressive flying tactics and OP-tempo as he called it then mechanical error.
I'm wondering if it maybe isn't a bit of both?
In layman's terms, what was the hardest thing about adapting to flying a Blackhawk? And how did that play into learning the fly more aggressively at the same time?
Lastly, I would love to hear some examples of the development of aggressive flying tactics?
Any help would be much appreciated.
I have been reading about the creation of TF-160 in the book, The Night Stalkers, by Durant, Hartov and Col. Johnson. In it, they discuss how there were growing pains with the Blackhawks during fast and low training missions and that some pilots and machines were lost.
I asked if some of these losses had anything to do with differences in flying a Blackhawk versus a Chinook or a Huey. Was there an adjustment period pilots experienced because of the Hawks engines, or rotor blades? Was there a difference in rotor RPM (is that a thing) or maybe the power to weight ratio that took some getting used to.
One person told me that one aspect of the Hawk that took some adjustment was the inertia of the rotor head. As a civilian I have no idea what that means. The same gentleman said the the Hawk also had more tail rotor authority. I assume that means it was more responsive and took some getting used to.
Another individual said the loss in Hawks in the beginning of TF-160 was more about the development of new, more aggressive flying tactics and OP-tempo as he called it then mechanical error.
I'm wondering if it maybe isn't a bit of both?
In layman's terms, what was the hardest thing about adapting to flying a Blackhawk? And how did that play into learning the fly more aggressively at the same time?
Lastly, I would love to hear some examples of the development of aggressive flying tactics?
Any help would be much appreciated.