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UDMH
UDMH Unsymmetrical dimethylhydrazine (UDMH) (1,1-Dimethylhydrazine) is a hypergolic rocket ... in combination with the oxidiser, nitrogen tetroxide. UDMH is toxic, a carcinogen and can explode ... there was concern about the levels of UDMH in various foods being a cancer risk, especially for apple juice. UDMH is also used as a nitrogen ...
http://en.wikipedia.org/wiki/UDMH - 1k - Cached - Similar pages
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Proton rocket
... 124 seconds Fuels N 2 O 4 /UDMH 2 - Core Stage Engines 4 RD ... 206 seconds Fuels N 2 O 4 /UDMH 3 - 3rd Stage Engine 1 RD ... 238 seconds Fuels N 2 O 4 /UDMH 4 - Blok D Stage Engine 1 ... m Length: 21.20 m Propellants: N2O4/UDMH Engines: 6 x RD-253-11D48 Other ... m Length: 14.00 m Propellants: N2O4/UDMH Engines: 4 RD-0210 Other designations: ...
http://en.wikipedia.org/wiki/Proton_rocket - 11k - Cached - Similar pages
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Unsymmetrical dimethylhydrazine (translated from Russian)
Unsymmetrical dimethylhydrazine Unsymmetrical dimethylhydrazine (UDMH) (1,1- dimethylhydrazine) (CH 3 ) 2 N ... ships, sputnikov , orbital'nykh and mezhplanetnykh stations . UDMH - colorless transparent liquid with the sharp unpleasant ... begin the loss of consciousness. The advantages UDMH + AT include: it exceeds the pair of ... filled form at normal temperatures The deficiencies UDMH + AT include: the toxicity carcinogenicity the probability of explosion UDMH in the presence of the oxidizer ...
http://ru.wikipedia.org/wiki/Несимметричный_диметилг ... - 4k - Cached (Russian) - Wikipedia (Russian) - Similar pages
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Apollo Command/Service Module
... engines CM RCS (N 2 O 4 /UDMH) x 12: 92 lbf ea 409 N SM RCS (N 2 O 4 /UDMH) x 16: 100 lbf ea 445 N ... N RCS propellants: N 2 O 4 /UDMH RCS engine propellants: 122 kg Drinking water ... tanks. The engine used Aerozine 50 (hydrazine/UDMH) fuel and nitrogen tetroxide oxidizer and had ... thrust: 16 x 446 N Propellants: N2O4/UDMH Service Propulsion (SPS) engine mass: 3, ...
http://en.wikipedia.org/wiki/Apollo_Command/Service_Module - 42k - Cached - Similar pages
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Apollo spacecraft
... N RCS Propellants: N 2 O 4 /UDMH RCS Engine Propellants: 75 kg RCS Specific ... 440 N Propellants: N 2 O 4 /UDMH RCS Specific Impulse I sp : 290 s ... Engine Propellants: N 2 O 4 /Aerozine_50 (UDMH/N2H4) SPS Engine Propellants: 18,413 kg ... kN RCS Propellants: N 2 O 4 /UDMH RCS Specific Impulse I sp : 290 s ... Engine Propellants: N 2 O 4 /Aerozine_50 (UDMH/N2H4) Ascent Engine Engine Isp: 311 ...
http://en.wikipedia.org/wiki/Apollo_spacecraft - 19k - Cached - Similar pages
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Proton (rocket) (translated from German)
... and 21 m for the fuel portion UDMH and 6 external tanks for the fuel ... Triebwerk. Both second, and third stage burn UDMH and Nitrogen tetroxide as fuel. For reaching ... Pay load: approx.. 12 t (NEO) Fuel: UDMH/NTO (asymmetrical Dimethylhydrazin /Nitrogen tetroxide) Proton K ... interplanetary), approx.. 2.6 t (GEO) Fuel: UDMH/NTO (asymmetrical Dimethylhydrazin/Distickstofftetroxid) Proton M Stages ... interplanetary), approx.. 3.2 t (GEO) Fuel: UDMH/NTO (asymmetrical Dimethylhydrazin/Distickstofftetroxid) Web on ...
http://de.wikipedia.org/wiki/Proton_(Rakete) - 15k - Cached (German) - Wikipedia (German) - Similar pages
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Liquid rocket propellants
... 1.22 1770 N 2 H 4 /UDMH 50/50 2831 1.98 3095 1 ... 51 3026 1.20 1775 IRFNA IIIa UDMH/DETA 60/40 2638 3.26 2848 ... 3178 2.71 2841 1.28 1655 UDMH 2668 3.13 2874 1.26 1648 ... 2864 1.27 1634 IRFNA IV HDA UDMH/DETA 60/40 2689 3.06 2903 ... 3242 2.58 2947 1.31 1680 UDMH 2719 2.95 2983 1.28 ...
http://en.wikipedia.org/wiki/Liquid_rocket_propellants - 23k - Cached - Similar pages
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Long March 2 rocket family
... kN Burn time 128 seconds Fuels N2O4 / UDMH 1 - Core Stage Engines YF - 20B x ... kN Burn time 166 seconds Fuels N2O4 / UDMH 2 - 2nd Stage Engine YF - 25/23 ... m Length: 15.3 m Propellants: N2O4 / UDMH Engines: 1 x YF - 20B per booster ... m Length: 23.7 m Propellants: N2O4 / UDMH Engine: 4 x YF - 20B Stage number ...
http://en.wikipedia.org/wiki/Long_March_2_rocket_family - 5k - Cached - Similar pages
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Apollo Lunar Module
... engines LM RCS (N 2 O 4 /UDMH) x 16: 100 lbf ea 441 N ... 445 N; four quads RCS propellants: N2O4/UDMH RCS specific impulse: 2.84 kNs/kg ... propellants: N 2 O 4 /Aerozine 50 (UDMH/N2H4) APS pressurant: 2 x 2.9 ... propellants: N 2 O 4 /Aerozine 50 (UDMH/N 2 H 4 ) DPS pressurant: 1 ...
http://en.wikipedia.org/wiki/Apollo_Lunar_Module - 28k - Cached - Similar pages
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Project Apollo
... engines CM RCS (N 2 O 4 /UDMH) x 12: 92 lbf ea 412 N SM RCS (N 2 O 4 /UDMH) x 16: 100 lbf ea 441 N ... Service Propulsion System (N 2 O 4 /UDMH) x 1: 22,000 lbf ea 97 ... engines LM RCS (N 2 O 4 /UDMH) x 16: 100 lbf ea 441 N ...
http://en.wikipedia.org/wiki/Project_Apollo - 53k - Cached - Similar pages
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