![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#15
|
|||
|
|||
![]()
Bill Daniels wrote:
OK, crank these numbers. Consider my Nimbus 2C (Experimental, so I could install a BRS) at 650 Kilos with water (which takes 5 minutes to dump). The gear strut will give 30mm on impact and the tire will give 50mm more. The cockpit shell is just fiberglass with no crush structure. I pop a BRS at 300 meters AGL with the surface wind at 15 knots. What are my chances? Give BRS weights, 'chute diameters and descent rates. My understanding is the "whole glider" German rescue systems will lower the glider nose down at about 40 degrees or so. If it is more level, it is likely to oscillate wildly so much the descent and impact can't be controlled. So, the landing gear is irrelevant, but the cockpit structure is extremely important. The nose must absorb the "landing". A Nimbus 2 might be a poor candidate for installing a system that won't be tested, except when you really need it. Your safety might be better served by selling the Nimbus and buying newer glider with a more crash tolerant cockpit. At least in the US, crashing while landing (meaning the last 100' of altitude) still claims more pilots than unsuccessful bailouts. -- ----- change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 02:26 PM |
Parachute fails to save SR-22 | Capt.Doug | Piloting | 72 | February 10th 05 05:14 AM |
Puchaz spin count 23 and counting | henell | Soaring | 116 | February 20th 04 12:35 AM |
Cessna 150 Price Outlook | Charles Talleyrand | Owning | 80 | October 16th 03 02:18 PM |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Piloting | 25 | September 11th 03 01:27 PM |