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1
OK my dear Borovik,

and I think that I have a real picture to it,but where ?.
2
Space Projects / Re: US Space Shuttle Projects
« Last post by hesham on Today at 05:11:44 am »
Hi,

did we send it here before ?.

http://p-d-m.livejournal.com/502215.html
3
Thank you my dear Borovik,

and can I ask you if there was a drawing survivor to La.172 ?.
I do not have any photos or any scheme La-172 (airplane with swept wing equipped with an engine RD-500, Derwent-V) ((
5
Postwar Aircraft Projects / Re: Myasishchev M-32
« Last post by hesham on Today at 05:00:50 am »
Amazing Info my dear Borovik.
6
Missile Projects / Re: Iraq's Full Final and Complete Disclosure
« Last post by Temistocle on Today at 04:58:08 am »
Dear all,
I just asked to the UN archives the access to the Iraq missile FFCD, the last one provided in 1996. They replied that I have to wait

30 years if the document is considered "confidential"
60 years if considered "strictly confidential"

but... starting from 2008 !!! So the 1996 missile FFCD will be more than 50 years old if released in 2038 (if the considered it only confidential). 

More information can be found here:

http://www.un.org/ga/search/view_doc.asp?symbol=ST/SGB/2009/12.

Section 6, in particular, outlines the conditions for early access to these records.
So, if you are not a member of the International Atomic Energy Agency (IAEA), the Organization for the Prohibition of Chemical Weapons (OPCW), the United Nations Environment Programme (UNEP) or the World Health Organization (WHO), you have to wait a loooong time.

Cheers

Temistocle
7
Postwar Aircraft Projects / Re: Soviet SST designs from the '60s
« Last post by borovik on Today at 04:50:08 am »
8
Postwar Aircraft Projects / Re: Myasishchev M-32
« Last post by borovik on Today at 04:37:23 am »
Also:



Far supersonic twin-engine bomber with delta wing "32" had a higher lift-drag ratio at supersonic speeds and better weight returns. Range 8400-8700 km at cruising speed with the number of M> 1.1, maximum speed 1850 km/h. In February 1953 preliminary design was sent to the MAP. To study the characteristics of an aircraft with a delta wing of small aspect ratio, an improved version of the YAK-1000M, the M-33 fighter, was also designed. The results obtained in the development of these projects were helpful when creating a new machine.

Source: http://www.khrunichev.ru/main.php/download/download/main.php?id=19&nid=27


I don't have any picture of the M-33 fighter design... Can anyone help on this one??
In addition to the bomber tailless with the same designation was a project of a small experimental aircraft M-33, not a fighter.
Quote
...aircraft project M-33 (March, 1951) is, in fact, a further development of the project Yak-1000, developed by L. Selyakov in OKB Yakovlev.
In the OKB-23 Myasishchev aircraft intended to be used as a pilot for studying the characteristics of a triangular wing of small aspect ratio at transonic speeds...
Иллюстрированная энциклопедия самолётов Мясищева том 2 часть 2.
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