I just can't wait for my "super hawk" natops and the amazing shit show that it will no doubt be.
A CH-53K is going to be able to carry a 27K external load out to a LZ 110NM away at 3000' at 94 degrees, loiter for 30 min with the load, drop the load and then fly back to the starting point and have 20 minutes on that end.
We currently have a newly minted O-4 with 90+ tow hours in the S at our squadron for trusted agent training. Regarding towing with the S, he remarks "the airframe isn't really suited for it."I know their testing in Pax. Anyone have any idea how that's going or when the OAMCM capability will make it to the fleet?
That's more to do with the debacle that is the LCS program than anything else. Stop-work orders tend to make lots of people mad.http://www.defenseindustrydaily.com/us-navys-top-acquisition-official-steps-down-03961/
I'm not sure what these means for the future our future but the Navy's head of acquisitions has decided to step down.
While the S for damn sure can't do the VOD mission that 53s do, they're doing their damndest to make it do the AMCM mission. The phrase "square peg in a round hole" comes to mind.Took this from another thread:
http://www.news.navy.mil/search/print.asp?story_id=32501&VIRIN=51590&imagetype=1&page=1
It specifically mentions....
"MH-60Rs and MH-60Ss will eventually replace all SH-60B, SH-60F, HH-60H, HH-1N, UH-3H and CH-46D helicopters currently in the Navy�s inventory, effectively increasing capability and flexibility."
The -53 isn't listed. Perhaps they are realistic about the S not being able to fulfill the role of the 53E.
The -53 isn't listed. Perhaps they are realistic about the S not being able to fulfill the role of the 53E.
Interesting article on the V-22 program.
http://www.time.com/time/magazine/article/0,9171,1666282,00.html
On the CH-47, no it can do what a CH-53E can do now lift wise nor can it do what a CH-53K will be able to do. It definitely is not shipboard compatible, blades do not fold except manually but the real show stopper is the aft pylon is too tall even for a CVN to get it off an elevator into the hangar. Efficiency at a high-density altitude is a different story.
Why would you want to interject something different in the supply chain with respect to a "new" medium lift aircraft? Buying the "K" makes sense logistically. Yes the "K" timeline could slide right, and the CH-53E will be the heavy lift until the "K" makes it. Compared to Joint Heavy Lift, the "K" is light years ahead, it is not a science project, and JHL is. Cost per flight hour on the 53E has dropped immensely. IMDS will further decrease that cost per flight hour. Whip out the Sling Load Manual and start looking at the weights of vehicles, conex boxes, and equipment and you will quickly see stuff weighs a lot. Things are only getting heavier from JSF engines to vehicles, so why buy a small truck where you do not have any room to grow payload wise? That is why you go big so you have the ability to meet future unforeseen needs.