Major Programmes for 2010-2011
Integration and launch of PSLV Flights PSLV-C16 (Resourcesat-
2, XSAT, Youthsat), PSLV-C17 (RISAT-1), PSLV-C18 (Megha-
Tropiques), PSLV-C19 (SRE-2, PROTIERS) and PSLV-C20
(SARAL, SAPPHIRE, NLS-7)
On the PSOM-XL motor fabricated by Ramakrishna Engineering Company, Veeraraghavan said while the six solid propellant strap-on motors in the standard PSLV carried nine tonnes of propellant, the new version PSOM-XL with a length of 13.5 metre had the capacity to carry a 12-tonne propellant. It would boost the capability of PSLV from 1,450 kg to 1,750 kg for a sun synchronous orbit. The motor will be used in the launch of PSLV C18 and PSLV C19 in the middle of next year, he added.
Nanosatellite Launch Service 7 and 9
PSLV-C19
Time frame: 2011 Q3
Orbit Parameters: SSO, 635-670 km, 09:00-10:30LTDN
NLS-7: SFL Spacecraft: CanX-4, CanX-5
NLS-9: Partner Spacecraft (To be finalised this fall)
Nanosatellite Launch Service 8 (NLS-8)
PSLV-C20
Timeframe: mid-2011
Orbit Parameters: SSO, 800 km, 06:00 LTDN
SFL Spacecraft: CanX-3A/UniBRITE,CanX-3B/BRITE-Austria
There is no such rocket designated with that number.
Resourcesat-2 Satellite Launch In January
In the referenced article it is written
"top space scientists would meet on December 10 to conduct a mission-readiness review and give the final go-ahead for the launch on December 20."
Does "December 20" refer to the final go-ahead or to the launch?
Is it one meeting or two?
I understand that there is a meeting on December 10, and the launch on December 20.
Do you share my view?
GSAT-5 PRIME
GSAT-5P is being planned as replacement for INSAT-3E and will carry 24 Normal C Band and 12 Extended C Band transponders with India Coverage. The spacecraft will be positioned at 55 deg East longitude with a mission life of 12 years.
The spacecraft weighs 2330 kg and payload power requirement is 1700W. Spacecraft configuration and equipment panel layouts are finalised. Payload subsystems and other subsystem packages are under advanced stage of realisation.
GSAT-5/INSAT-4D
Configured as an exclusive C-band communication satellite, GSAT-5/INSAT-4D will carry 12 normal C-band transponders and six extended C-band transponders with wider coverage in uplink and downlink over Asia, Africa and Eastern Europe as well as zonal coverage with a minimum of 35 dBW EIRP.
The spacecraft has a mission life of 12 years. The spacecraft weighs 2330 kg and has a power generation capability of 2000W. The layouts for all equipment panels are finalised. Fabrication of bus system elements have been initiated.
GSAT-5P
Configured as an exclusive C-band communication satellite, GSAT-5P/INSAT-4D will carry 12 normal C-band transponders and 6 extended C-band transponders with wider coverage in uplink and downlink over Asia, Africa and Eastern Europe as well as zonal coverage with a minimum of 35 dBW EIRP. The spacecraft has a mission life of 12 years and planned to be launched onboard GSLV-F06.
The two cube-shaped satellites -- each measuring just 20 centimetres (eight inches) per side and weighing seven kilograms (15 pounds) -- are part of a joint project with Canada and Poland entitled "BRITE" (Bright Target Explorer).
The Austrian satellites will be launched aboard an Indian rocket in late July, although a clear date as not yet been set.
Four further satellites, two from Poland and two from Canada, will then follow in 2012.
May 19, 2010, a press conference was held in the Ministry of Science and Higher Education. The first model of satellite BRITE-PL was presented during this conference. An annex to the agreement on the financing of the project to build and launch satellites was also signed then.
The first Polish satellite will be placed in orbit in 2011 and a second in 2013.
http://isro.org/news/pdf/gslvf06-gsat5p.pdf
GSLV-F06 will fly with russian C15 upper stage. It is a first indo-russian GSLV MkII.