ML19256D306

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Summary of 680315 Telcon W/Naval Ordnance Lab & Gilbert Associates,Inc Re Aircraft Impact Analysis Underway for Facility
ML19256D306
Person / Time
Site: Crane Constellation icon.png
Issue date: 03/22/1968
From: Grimes B
US ATOMIC ENERGY COMMISSION (AEC)
To:
US ATOMIC ENERGY COMMISSION (AEC)
References
NUDOCS 7910170814
Download: ML19256D306 (2)


Text

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de. rived from a Ccr.vair 3U0 (2CO,0C0 1;) cr:.sa study recen:1 c:rpla c.i C;nvair and 7.u.

Mr. John.ioracrc, Chie f o f :he S truc tures In;incerin 5

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The loadin; for che 3ccing 707 (3CC,000 lb) prope:ed cy :he 2p-licant pea. c at abou: /.J ' ; (as opposed to the previcur 20'g ac cu--:1cn).

(::c te : Thu wa.: later chan?cd to e. '.s at abcut 70; cn.;2rch 22,1. c.)

Mr. Craneburger said that the previcus analysis had 2: uced a E dar-ir :

value e:: cept a: the area of in,act ' : era 1Z. v2: ssured but tha: the fin:.

analysn would prchably use a 1cuer d:= pin' /21ue. The ' failure p o in t assumed aas the top layer of concrete failing in ccmprescian. When asked whether the juncticn of doce and cylinder wculd be a limiting poin:.ith respect to impact capability of the centainment, Mr, Croneburger sci; : hat the structure weu'.

'cc s tif fer and that th;re ;; 2 greater =2;; at th_.

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for the above table ir tha: the planc crucac thrcush cu::e;-

The ratienale the -lanc ac t:

danse structures and when the win;s arc reached, sively scr2 rac id i,r c t e - r. e d. T h 2,.

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ure and :he o'.2nc

_3 f;r a 707 -. f;r a ri'ia the same decelcration anc pre:;ure valuc; cu.d ap?(

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a C5A althau ;h tha total load ucull be smaller (since the :rc;;ura i.

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.se Fcr a 707 the times in the lead ta'a.e ac:ve ueu.-

over a c: aller arca).

factor of about 1.5 since the '.en; h; :: the planes hava to be adjust 2d by a proportion and the wing strue:ure of the 707 wou'.d be rcachc.

are in that cocner.

If the above corrections for weight and time are made, the L;ckheed table D lb at 0.29 seccnds. This is quite would give a peak loading of 21 x 10

106 15 at 0.lc5 ceconds preposed different frca the peak loadin; of 12.5 to 21.2 The 7ea'.; leading was later increased by,the ap?licant.

(Note:

10 lb at 0.21 sec.)

Mr. Cronobur;er indicated he would pursue that calculatica using his cwn these loading facters wi:h cur other loading factors. We will discuss censultants.

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