|
gptkbp:instance_of
|
gptkb:drones
|
|
gptkbp:can_be_configured_for
|
multiple payloads
|
|
gptkbp:challenges
|
thermal protection
|
|
gptkbp:collaborated_with
|
various aerospace companies
|
|
gptkbp:competitors
|
gptkb:Rocket_Lab_Electron
gptkb:Space_X_Falcon_9
|
|
gptkbp:control_system
|
autonomous guidance
autonomous flight control
|
|
gptkbp:customer_base
|
commercial and government
|
|
gptkbp:customer_support
|
gptkb:NASA
|
|
gptkbp:debut
|
ongoing
|
|
gptkbp:design
|
5 years
|
|
gptkbp:developed_by
|
gptkb:USA
gptkb:Firefly_Aerospace
|
|
gptkbp:development
|
Firefly Aerospace engineers
|
|
gptkbp:development_cost
|
$75 million
|
|
gptkbp:diameter
|
2.5 m
|
|
gptkbp:durability
|
no
|
|
gptkbp:elevation
|
20 meters
|
|
gptkbp:engine
|
gptkb:Firefly_Aerospace
|
|
gptkbp:engine_configuration
|
staged combustion
|
|
gptkbp:engine_type
|
gptkb:RP-1/_LOX
staged combustion engine
|
|
gptkbp:environmental_concerns
|
low emissions
|
|
gptkbp:first_flight
|
gptkb:2021
2021-09-11
scheduled for 2024
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:funding
|
gptkb:venture_capital
|
|
gptkbp:future_plans
|
expand launch capabilities
expand payload capacity
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:has_a_focus_on
|
cost efficiency
|
|
gptkbp:has_development_timeline
|
2014-2024
|
|
gptkbp:has_height
|
20 m
|
|
gptkbp:has_launch_frequency
|
monthly
|
|
gptkbp:has_launch_partner
|
various commercial customers
|
|
gptkbp:has_max_payload_to_leo
|
1000 kg
|
|
gptkbp:has_mission
|
dedicated launches
|
|
gptkbp:has_payload_fairing
|
gptkb:textiles
|
|
gptkbp:height
|
3.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Firefly V2
|
|
gptkbp:is_anticipated_by
|
gptkb:space_enthusiasts
|
|
gptkbp:is_designed_for
|
small satellite launches
|
|
gptkbp:is_part_of
|
gptkb:Alpha_rocket_family
commercial space industry
small satellite launch market
|
|
gptkbp:is_promoted_by
|
Firefly Aerospace marketing
|
|
gptkbp:is_supported_by
|
venture capital funding
NASA contracts
|
|
gptkbp:is_tested_for
|
reliability
static fire tests
simulated payloads
Space X facilities
|
|
gptkbp:is_used_for
|
orbital missions
|
|
gptkbp:is_utilized_by
|
startups and universities
|
|
gptkbp:launch_date
|
2024
up to 24 per year
|
|
gptkbp:launch_price
|
$15 million
|
|
gptkbp:launch_site
|
gptkb:Vandenberg_Space_Force_Base
|
|
gptkbp:launch_vehicle
|
gptkb:Alpha
gptkb:Team_Rocket
modular design
vertical takeoff
small launch vehicle
|
|
gptkbp:launch_vehicle_width
|
4 meters
|
|
gptkbp:launch_window
|
year-round
2023-2024
|
|
gptkbp:manufacturer
|
gptkb:Firefly_Aerospace
|
|
gptkbp:max_thrust
|
500 k N
|
|
gptkbp:mission
|
dedicated launches
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operated_by
|
RP-1 and Liquid Oxygen
|
|
gptkbp:operational_range
|
low Earth orbit
|
|
gptkbp:operational_status
|
planned
|
|
gptkbp:orbit_type
|
sun-synchronous orbit
|
|
gptkbp:partnerships
|
various aerospace companies
|
|
gptkbp:payload_capacity
|
2.5 meters
1500 kg
ground support equipment
|
|
gptkbp:payload_deployment_method
|
separation system
|
|
gptkbp:produced_by
|
gptkb:Firefly_Aerospace
|
|
gptkbp:production_status
|
in development
|
|
gptkbp:propulsion
|
> 100:1
|
|
gptkbp:public_interest
|
high
|
|
gptkbp:purpose
|
gptkb:Space_Launch_System
|
|
gptkbp:regulatory_compliance
|
FAA regulations
|
|
gptkbp:released
|
2024
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:specification
|
available online
|
|
gptkbp:target_market
|
small satellite launches
|
|
gptkbp:bfsParent
|
gptkb:Firefly
gptkb:Razer_Firefly
|
|
gptkbp:bfsLayer
|
5
|