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Launch window: 7:20 pm local time (10:20 p.m. EDT)
Launch site: SLC-2W, Vandenberg Air Force Base, California
The United Launch Alliance Delta 2 rocket will launch the fourth Italian COSMO-SkyMed radar Earth-imaging satellite. The X-Band Synthetic Aperture Radar payload on the spacecraft will be used for civil and military applications. The rocket will fly in the 7420-10 vehicle configuration. ULA will conduct this commercial launch for Boeing.
Live Stream: http://www.ulalaunch.com/site/pages/Webcast.shtml
ULA's Launch Info: http://www.ulalaunch.com/site/pages/Launch.shtml#/12/ (not yet available)
COSMO-SkyMed Wikipedia Article: http://en.wikipedia.org/wiki/COSMO-SkyMed
Gunter's Space Page COSMO-SkyMed Page: http://space.skyrocket.de/doc_sdat/cosmo-skymed-1.htm
Astronautix COSMO-SkyMed Page: http://www.astronautix.com/craft/coskymed.htm
Thales GROUP COSMO-SkyMed Page: http://www.thalesgroup.com/News_and_eve ... smoSkymed/
Delta II Launch Vehicle
ULA's Delta II Page: http://www.ulalaunch.com/site/pages/Pro ... taII.shtml
Delta II Product Card: http://www.ulalaunch.com/site/docs/prod ... t_card.pdf
Delta II Product Guide: http://www.ulalaunch.com/site/docs/prod ... de2007.pdf
Boeing Delta II Page: http://www.boeing.com/defense-space/spa ... delta2.htm
Delta II Wikipedia Article: http://en.wikipedia.org/wiki/Delta_II
Vandenberg AFB Delta II Page: http://www.vandenberg.af.mil/library/fa ... sp?id=5206
Delta II Flight Configuration Key: 7X2Y-ZZ
7=7000 series (nowadays always 7), last 6000 series flown in 1992
X=Number of GEMs (Graphite Epoxy Motor), either 3, 4 or 9.
2=Type of Second Stage (nowadays always 2=Aerojet AJ10). Only Deltas prior 6000 used TR-201 engine.
Y=Type of Third Stage, either 0 (=no third stage), 5 (=Star 48B) or 6 (=Star 37FM).
ZZ=Type of payload fairing, aluminum fairing 9,5ft in diameter, 10ft fairing made of composite or lengthened 10ft fairing.
There is also 792xH series Delta II rocket where H means heavy version. Three of its nine GEMs are bigger GEM-46 instead regular GEM-40.
Performance of Different Delta II Models:
732X-10: 2550kg LEO, 880kg GTO
742X-10: 2920kg LEO, 1010kg GTO
792X-10: 4590kg LEO, 1710kg GTO
792XH-10: 5520kg LEO, 2040kg GTO
Geosynchronous transfer orbit (GTO): 35786 x 185 km (19323 x 100 nmi) at 28.7°
Low-Earth orbit (LEO): 407 km (220 nmi) circular at 28.7°
Delta II First Stage
One RS-27A engine burning RP-1/LOX
RS-27A Wikipedia Article: http://en.wikipedia.org/wiki/RS-27A
P&W Rocketdyne Rs-27A Page: http://www.pw.utc.com/vgn-ext-templatin ... 62529fRCRD
P&W Rocketdyne RS-27A Fact Sheet: http://www.pw.utc.com/StaticFiles/Pratt ... RS-27A.pdf
Purdue University's RS-27A Page: https://engineering.purdue.edu/AAE/Rese ... ids/rs27a/
NASA's RS-68 Test Program: http://sscfreedom.ssc.nasa.gov/etd/ETDP ... S_RS68.asp
Delta II Boosters
Delta II 7420 has four GEM-40 (Graphite Epoxy Motor) booster rockets which use solid fuel.
GEM Wikipedia Article: http://en.wikipedia.org/wiki/Graphite-Epoxy_Motor
GEM-40 in ATK Product Catalog: http://www.atk.com/capabilities_space/d ... df#page=29
Delta II Second Stage
One Aerojet AJ10 engine burning N[sub]2[/sub]O[sub]4[/sub]/Aerozine 50
AJ-10 Wikipedia Article: http://en.wikipedia.org/wiki/AJ-10
Purdue University's AJ-10 Page: http://cobweb.ecn.purdue.edu/~propulsi/ ... -118k.html
Aerojet Spacelift Propulsion Page: http://www.aerojet.com/capabilities/spacelift.php
Astronautix AJ-10 Page: http://www.astronautix.com/engines/aj10118k.htm
Vandenberg Air Force Base
Vandenberg AFB Wikipedia Article: http://en.wikipedia.org/wiki/Vandenberg_Air_Force_Base
SLC-2 Wikipedia Article: http://en.wikipedia.org/wiki/Vandenberg ... _Complex_2
Astronautix SLC-2W Page: http://www.astronautix.com/sites/vanslc2w.htm
Vandenberg AFB Official SLC-2 Photos: http://www.vandenberg.af.mil/photos/med ... 5&btnG.y=3
Vandenberg AFB Google Maps Link: http://maps.google.com/maps?ll=34.72972 ... 120.576944
SLC-2 Google Maps Link: http://maps.google.com/maps?ll=34.7545, ... ,-120.6198
Launch site: SLC-2W, Vandenberg Air Force Base, California
The United Launch Alliance Delta 2 rocket will launch the fourth Italian COSMO-SkyMed radar Earth-imaging satellite. The X-Band Synthetic Aperture Radar payload on the spacecraft will be used for civil and military applications. The rocket will fly in the 7420-10 vehicle configuration. ULA will conduct this commercial launch for Boeing.
Live Stream: http://www.ulalaunch.com/site/pages/Webcast.shtml
ULA's Launch Info: http://www.ulalaunch.com/site/pages/Launch.shtml#/12/ (not yet available)
COSMO-SkyMed Wikipedia Article: http://en.wikipedia.org/wiki/COSMO-SkyMed
Gunter's Space Page COSMO-SkyMed Page: http://space.skyrocket.de/doc_sdat/cosmo-skymed-1.htm
Astronautix COSMO-SkyMed Page: http://www.astronautix.com/craft/coskymed.htm
Thales GROUP COSMO-SkyMed Page: http://www.thalesgroup.com/News_and_eve ... smoSkymed/
Delta II Launch Vehicle
ULA's Delta II Page: http://www.ulalaunch.com/site/pages/Pro ... taII.shtml
Delta II Product Card: http://www.ulalaunch.com/site/docs/prod ... t_card.pdf
Delta II Product Guide: http://www.ulalaunch.com/site/docs/prod ... de2007.pdf
Boeing Delta II Page: http://www.boeing.com/defense-space/spa ... delta2.htm
Delta II Wikipedia Article: http://en.wikipedia.org/wiki/Delta_II
Vandenberg AFB Delta II Page: http://www.vandenberg.af.mil/library/fa ... sp?id=5206
Delta II Flight Configuration Key: 7X2Y-ZZ
7=7000 series (nowadays always 7), last 6000 series flown in 1992
X=Number of GEMs (Graphite Epoxy Motor), either 3, 4 or 9.
2=Type of Second Stage (nowadays always 2=Aerojet AJ10). Only Deltas prior 6000 used TR-201 engine.
Y=Type of Third Stage, either 0 (=no third stage), 5 (=Star 48B) or 6 (=Star 37FM).
ZZ=Type of payload fairing, aluminum fairing 9,5ft in diameter, 10ft fairing made of composite or lengthened 10ft fairing.
There is also 792xH series Delta II rocket where H means heavy version. Three of its nine GEMs are bigger GEM-46 instead regular GEM-40.
Performance of Different Delta II Models:
732X-10: 2550kg LEO, 880kg GTO
742X-10: 2920kg LEO, 1010kg GTO
792X-10: 4590kg LEO, 1710kg GTO
792XH-10: 5520kg LEO, 2040kg GTO
Geosynchronous transfer orbit (GTO): 35786 x 185 km (19323 x 100 nmi) at 28.7°
Low-Earth orbit (LEO): 407 km (220 nmi) circular at 28.7°
Delta II First Stage
One RS-27A engine burning RP-1/LOX
RS-27A Wikipedia Article: http://en.wikipedia.org/wiki/RS-27A
P&W Rocketdyne Rs-27A Page: http://www.pw.utc.com/vgn-ext-templatin ... 62529fRCRD
P&W Rocketdyne RS-27A Fact Sheet: http://www.pw.utc.com/StaticFiles/Pratt ... RS-27A.pdf
Purdue University's RS-27A Page: https://engineering.purdue.edu/AAE/Rese ... ids/rs27a/
NASA's RS-68 Test Program: http://sscfreedom.ssc.nasa.gov/etd/ETDP ... S_RS68.asp
Delta II Boosters
Delta II 7420 has four GEM-40 (Graphite Epoxy Motor) booster rockets which use solid fuel.
GEM Wikipedia Article: http://en.wikipedia.org/wiki/Graphite-Epoxy_Motor
GEM-40 in ATK Product Catalog: http://www.atk.com/capabilities_space/d ... df#page=29
Delta II Second Stage
One Aerojet AJ10 engine burning N[sub]2[/sub]O[sub]4[/sub]/Aerozine 50
AJ-10 Wikipedia Article: http://en.wikipedia.org/wiki/AJ-10
Purdue University's AJ-10 Page: http://cobweb.ecn.purdue.edu/~propulsi/ ... -118k.html
Aerojet Spacelift Propulsion Page: http://www.aerojet.com/capabilities/spacelift.php
Astronautix AJ-10 Page: http://www.astronautix.com/engines/aj10118k.htm
Vandenberg Air Force Base
Vandenberg AFB Wikipedia Article: http://en.wikipedia.org/wiki/Vandenberg_Air_Force_Base
SLC-2 Wikipedia Article: http://en.wikipedia.org/wiki/Vandenberg ... _Complex_2
Astronautix SLC-2W Page: http://www.astronautix.com/sites/vanslc2w.htm
Vandenberg AFB Official SLC-2 Photos: http://www.vandenberg.af.mil/photos/med ... 5&btnG.y=3
Vandenberg AFB Google Maps Link: http://maps.google.com/maps?ll=34.72972 ... 120.576944
SLC-2 Google Maps Link: http://maps.google.com/maps?ll=34.7545, ... ,-120.6198