Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Space_Launch_System
|
| gptkbp:academic_programs |
experienced aerospace engineers
|
| gptkbp:competitors |
growing competition in small launch market
|
| gptkbp:customer_base |
diverse global customers
|
| gptkbp:customer_satisfaction |
high customer satisfaction
|
| gptkbp:debut |
gptkb:2018
over 20 successful launches |
| gptkbp:development |
gptkb:2014
|
| gptkbp:durability |
partially reusable
|
| gptkbp:engine |
9 engines in first stage
|
| gptkbp:engine_type |
Rocket Lab Rutherford engine
|
| gptkbp:environmental_concerns |
focus on reducing environmental impact
|
| gptkbp:first_flight |
January 20, 2017
|
| gptkbp:fuel_type |
RP-1 and liquid oxygen
|
| gptkbp:future_plans |
expanding launch capabilities
|
| gptkbp:global_presence |
growing global presence in the launch market
|
| gptkbp:guidance_system |
gptkb:navigation_system
|
| gptkbp:height |
17 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Electron launch vehicle
|
| gptkbp:infrastructure |
Rocket Lab launch complex
|
| gptkbp:investment_focus |
small satellite launches
|
| gptkbp:launch_cadence |
increasing
|
| gptkbp:launch_date |
multiple launches per year
|
| gptkbp:launch_price |
approximately $7.5 million
|
| gptkbp:launch_site |
Māhia Peninsula, New Zealand
|
| gptkbp:launch_vehicle |
high reliability
expendable launch vehicle optimized for efficiency optimized for small payloads continuous innovation efforts planned upgrades for performance improvements Electron family |
| gptkbp:launch_window |
varies by mission
|
| gptkbp:manufacturer |
gptkb:Rocket_Lab
|
| gptkbp:market |
commercial satellite operators
|
| gptkbp:mission |
over 90% success rate
Rocket Lab mission control |
| gptkbp:mission_type |
dedicated and rideshare missions
|
| gptkbp:notable_mission |
Black Sky Global satellite launches
|
| gptkbp:number_of_stages |
2
|
| gptkbp:operational_status |
active
|
| gptkbp:orbit_type |
Low Earth Orbit (LEO)
|
| gptkbp:partnerships |
various aerospace partnerships
|
| gptkbp:payload_capacity |
1.2 meters
300 kg vertical integration multiple payloads in one launch |
| gptkbp:project |
developing new technologies for future missions
|
| gptkbp:propulsion |
24 k N per engine
|
| gptkbp:recovery_method |
planned for future versions
|
| gptkbp:release_country |
conducted internationally
|
| gptkbp:safety_record |
good
|
| gptkbp:success_rate |
high
|
| gptkbp:technology |
advanced propulsion technology
|
| gptkbp:bfsParent |
gptkb:Rocket_Lab_Mission_Control
|
| gptkbp:bfsLayer |
7
|