Statements (107)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:Space_Launch_System
|
gptkbp:collaboration |
gptkb:Limited
limited |
gptkbp:community_outreach |
Involvement in educational programs
|
gptkbp:configuration |
vertical launch
|
gptkbp:control_system |
digital control system
Active control system |
gptkbp:country |
gptkb:India
|
gptkbp:customer_base |
diverse customer base
|
gptkbp:debut |
gptkb:2022
gptkb:2023 Ongoing since 2021 |
gptkbp:design_features |
modular design
Compact and lightweight design |
gptkbp:design_purpose |
Cost-effective and reliable launches
|
gptkbp:designed_by |
gptkb:ISRO
gptkb:Indian_Space_Research_Organisation |
gptkbp:development |
gptkb:2018
gptkb:2019 ISRO engineers |
gptkbp:development_cost |
approximately $30 million
Approx. $30 million |
gptkbp:diameter |
2.5 meters
|
gptkbp:durability |
No
not reusable |
gptkbp:engine |
Indigenous development by ISRO
|
gptkbp:engine_type |
solid rocket motor
Liquid and solid propulsion |
gptkbp:environmental_impact |
low environmental impact
Minimized environmental impact |
gptkbp:first_flight |
August 7, 2022
August 7, 2021 Multiple pre-launch tests conducted |
gptkbp:fuel_type |
solid fuel
Kerosene and liquid oxygen |
gptkbp:future_plans |
expand capabilities
Expand payload capacity |
gptkbp:guidance_system |
gptkb:navigation_system
Inertial navigation system |
https://www.w3.org/2000/01/rdf-schema#label |
SSLV
|
gptkbp:integrates_with |
streamlined integration process
|
gptkbp:integration |
Short integration time
|
gptkbp:investment_focus |
Commercial satellite launches
|
gptkbp:involved_technology |
promotes technology transfer
Available for international customers |
gptkbp:launch_date |
up to 12 launches per year
Up to 6 times a year |
gptkbp:launch_event |
Successful initial missions
|
gptkbp:launch_frequency_goal |
increase launch frequency
|
gptkbp:launch_price |
Approx. $5 million per launch
approximately $5 million per launch |
gptkbp:launch_service_provider |
gptkb:ISRO
|
gptkbp:launch_site |
gptkb:Satish_Dhawan_Space_Centre
|
gptkbp:launch_vehicle |
gptkb:SSLV_family
small launch vehicles small satellite launch vehicle |
gptkbp:launch_window |
Flexible
flexible launch windows |
gptkbp:launched |
gptkb:Vertical
2 weeks Rapid launch preparation capability |
gptkbp:length |
34 meters
|
gptkbp:manufacturer |
gptkb:ISRO
|
gptkbp:market_position |
competitive
|
gptkbp:media_coverage |
Significant media coverage during launches
|
gptkbp:mission |
gptkb:ISRO_Telemetry,_Tracking_and_Command_Network
successful missions low Earth orbit missions diverse mission capabilities |
gptkbp:notable_launches |
gptkb:Earth_observation
|
gptkbp:number_of_engines |
gptkb:4
|
gptkbp:number_of_stages |
gptkb:3
|
gptkbp:operational_cost |
low operational cost
|
gptkbp:operational_status |
Active
active |
gptkbp:operational_use |
Used for commercial satellite deployment
|
gptkbp:orbit_type |
Low Earth orbit
Sun-synchronous orbit |
gptkbp:partnership |
established partnerships
|
gptkbp:partnerships |
Partnerships with private sector
|
gptkbp:payload_capacity |
500 kg to Sun-synchronous orbit
2.5 meters in diameter Quick payload integration process |
gptkbp:payload_integration_time |
short
|
gptkbp:primary_use |
small satellite launches
|
gptkbp:propulsion |
1000 k N
400 k N |
gptkbp:public_interest |
High public interest in launches
|
gptkbp:purpose |
Small satellite launch
|
gptkbp:reliability |
high reliability
High reliability expected |
gptkbp:research_and_development |
ongoing R& D efforts
|
gptkbp:safety_record |
good safety record
No failures reported |
gptkbp:success_rate |
high
100% in initial flights |
gptkbp:supports |
standardized equipment
|
gptkbp:target_market |
commercial satellite operators
|
gptkbp:upgrades |
planned upgrades
Potential for future upgrades |
gptkbp:user_countries |
gptkb:India
Various countries interested |
gptkbp:user_feedback |
positive user feedback
|
gptkbp:weight |
120 tons
|
gptkbp:bfsParent |
gptkb:ISRO
gptkb:Indian_Space_Research_Organisation |
gptkbp:bfsLayer |
4
|