Statements (55)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:Team_Rocket
|
gptkbp:collaboration |
with Russia
with France with the USA |
gptkbp:components |
gptkb:solid_rocket_boosters
cryogenic upper stage liquid core stage |
gptkbp:development |
1990s
|
gptkbp:first_cryogenic_flight |
GSLV-D5
|
gptkbp:first_flight |
gptkb:2001
gptkb:GSLV-D1 |
gptkbp:fuel_type |
UDMH and N2 O4
|
gptkbp:height |
approximately 49 meters
|
https://www.w3.org/2000/01/rdf-schema#label |
India's GSLV engine
|
gptkbp:launch_date |
several launches per year
|
gptkbp:launch_site |
gptkb:Satish_Dhawan_Space_Centre
|
gptkbp:manufacturer |
gptkb:ISRO
|
gptkbp:notable_achievement |
launching GSAT-6 A
launching GSAT-12 launching GSAT-15 launching GSAT-19 launching GSAT-29 launching GSAT-30 launching GSAT-31 launching GSAT-32 launching GSAT-33 launching GSAT-34 launching GSAT-35 launching GSAT-36 launching GSAT-37 launching GSAT-38 launching GSAT-39 launching GSAT-40 launching GSAT-41 launching GSAT-42 launching GSAT-43 launching GSAT-44 launching GSAT-45 launching GSAT-46 launching GSAT-47 launching GSAT-48 launching GSAT-49 launching GSAT-50 |
gptkbp:notable_launches |
gptkb:GSAT_series
|
gptkbp:operational_status |
active
|
gptkbp:payload_capacity |
up to 2,500 kg to GTO
|
gptkbp:propulsion |
80 k N
|
gptkbp:reliability |
improving over time
|
gptkbp:significance |
strategic for India's space program
|
gptkbp:successor |
gptkb:GSLV_Mk_III
|
gptkbp:type |
liquid-fueled engine
|
gptkbp:upgrades |
ongoing development
|
gptkbp:used_for |
launching satellites
|
gptkbp:bfsParent |
gptkb:AR1_rocket_engine
|
gptkbp:bfsLayer |
6
|