Z
Zipi
Guest
Information collected mainly from SiberianTiger's infopack: http://www.orbiter-forum.com/showthread.php?t=15440
Launch time: 01:05 A.M. UTC
Launch site: Plesetsk Launch Pad #132/1, 62°53'0.40"N, 40°52'6.43"E
Anticipated Payload: Parus military navigation/communication satellite
Payload:
Mass: 825 kg (1,818 lb).
Electrical System: Solar cells on exterior.
Electric System: 0.20 average kW.
Attitude keeping: Passive gravity gradient boom.
Parus satellite Wikipedia article: http://en.wikipedia.org/wiki/Parus_(satellite)
Satellite Manufacturer ISS-Reshetnev's Tsiklon page: http://www.iss-reshetnev.com/?cid=leoca&caid=2
Satellite Manufacturer ISS-Reshetnev's Tsikada page: http://www.iss-reshetnev.com/?cid=leoca&caid=15
Launch Vehicle:
Kosmos-3M Wikipedia Article: http://en.wikipedia.org/wiki/Kosmos-3M
RussianSpaceWeb Kosmos LV Family Page: http://www.russianspaceweb.com/cosmos3.html
Astronautix Kosmos-3 Page: http://www.astronautix.com/lvs/kosmos3.htm
Kosmos-3M Photo Gallery: http://polyot.su/main.php?id=138
Kosmos-3M Manufacturer's website: http://translate.google.com/translate?j ... l=ru&tl=en
(without Google Translation: http://polyot.su/)
Polyot's Kosmos-3M English Page: http://polyot.su/main.php?id=30&lang=en
Khrunichev Kosmos-3M English Page: http://www.khrunichev.ru/main.php?id=86&lang=en
Plesetsk Kosmos-3M Page: http://translate.googleusercontent.com/ ... kSV7seyxPQ
(without Google Translation: http://www.plesetzk.ru/rn/cosmos3)
Some Engine info from Buran-Energia: http://www.buran-energia.com/energia/mo ... moteur.php
Engine Comparisons: http://www.b14643.de/Spacerockets_1/Div ... ngines.htm
Engine Manufacturer NPO Energomash website: http://www.npoem.ru/eng/

First Stage:
One RD-216 engine burning IRFNA/UDMH.
Astronautix RD-216 Page: http://www.astronautix.com/engines/rd216.htm
Second Stage:
One RD-219 engine burning IRFNA/UDMH.
Astronautix RD-219 Page: http://www.astronautix.com/engines/rd219.htm
Launch time: 01:05 A.M. UTC
Launch site: Plesetsk Launch Pad #132/1, 62°53'0.40"N, 40°52'6.43"E
Anticipated Payload: Parus military navigation/communication satellite

Payload:
Mass: 825 kg (1,818 lb).
Electrical System: Solar cells on exterior.
Electric System: 0.20 average kW.
Attitude keeping: Passive gravity gradient boom.
Parus satellite Wikipedia article: http://en.wikipedia.org/wiki/Parus_(satellite)
Satellite Manufacturer ISS-Reshetnev's Tsiklon page: http://www.iss-reshetnev.com/?cid=leoca&caid=2
Satellite Manufacturer ISS-Reshetnev's Tsikada page: http://www.iss-reshetnev.com/?cid=leoca&caid=15

Launch Vehicle:
Kosmos-3M Wikipedia Article: http://en.wikipedia.org/wiki/Kosmos-3M
RussianSpaceWeb Kosmos LV Family Page: http://www.russianspaceweb.com/cosmos3.html
Astronautix Kosmos-3 Page: http://www.astronautix.com/lvs/kosmos3.htm
Kosmos-3M Photo Gallery: http://polyot.su/main.php?id=138
Kosmos-3M Manufacturer's website: http://translate.google.com/translate?j ... l=ru&tl=en
(without Google Translation: http://polyot.su/)
Polyot's Kosmos-3M English Page: http://polyot.su/main.php?id=30&lang=en
Khrunichev Kosmos-3M English Page: http://www.khrunichev.ru/main.php?id=86&lang=en
Plesetsk Kosmos-3M Page: http://translate.googleusercontent.com/ ... kSV7seyxPQ
(without Google Translation: http://www.plesetzk.ru/rn/cosmos3)
Some Engine info from Buran-Energia: http://www.buran-energia.com/energia/mo ... moteur.php
Engine Comparisons: http://www.b14643.de/Spacerockets_1/Div ... ngines.htm
Engine Manufacturer NPO Energomash website: http://www.npoem.ru/eng/


First Stage:
One RD-216 engine burning IRFNA/UDMH.
Astronautix RD-216 Page: http://www.astronautix.com/engines/rd216.htm


Second Stage:
One RD-219 engine burning IRFNA/UDMH.
Astronautix RD-219 Page: http://www.astronautix.com/engines/rd219.htm

