|
gptkbp:instance_of
|
gptkb:patent
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Mark_III_armor
|
|
gptkbp:aircraft_operated
|
30 days
|
|
gptkbp:avionics
|
advanced avionics
|
|
gptkbp:budget
|
$500 million
|
|
gptkbp:collaborations
|
gptkb:battle
international space agencies
|
|
gptkbp:collection
|
real-time data
|
|
gptkbp:communication
|
satellite communication
|
|
gptkbp:community_engagement
|
high
|
|
gptkbp:community_involvement
|
STEM programs
|
|
gptkbp:controls
|
autonomous navigation
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:4
simulator training
|
|
gptkbp:design
|
interplanetary travel
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:developer
|
2020-01-01
|
|
gptkbp:elevation
|
300 km
|
|
gptkbp:emergency_services
|
abort system
|
|
gptkbp:engine
|
gptkb:Rocketdyne
|
|
gptkbp:engine_type
|
gptkb:rocket
|
|
gptkbp:environmental_impact
|
completed
|
|
gptkbp:first_flight
|
gptkb:cape
gptkb:2023
2023-05-15
|
|
gptkbp:fuel_type
|
liquid oxygen
|
|
gptkbp:has_programs
|
gptkb:Artemis_Program
|
|
gptkbp:height
|
4 m
|
|
gptkbp:historical_significance
|
first prototype for Mars missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mark III Prototype
|
|
gptkbp:instrument
|
various payloads
|
|
gptkbp:is_a_supporter_of
|
planned for 2024
|
|
gptkbp:is_tested_for
|
ongoing
aerodynamic testing
|
|
gptkbp:is_used_for
|
gptkb:spacecraft
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
2500 kg
|
|
gptkbp:launched
|
2024-2025
|
|
gptkbp:length
|
15 m
|
|
gptkbp:manufacturer
|
gptkb:Space_Tech_Industries
|
|
gptkbp:max_speed
|
25000 km/h
|
|
gptkbp:max_takeoff_weight
|
parachute and thrusters
|
|
gptkbp:media_coverage
|
extensive
|
|
gptkbp:mission
|
gptkb:spacecraft
planned
Houston Control Center
|
|
gptkbp:objective
|
gptkb:Mars_exploration
lunar missions
|
|
gptkbp:partnerships
|
private sector partnerships
|
|
gptkbp:regulatory_compliance
|
pending
|
|
gptkbp:research_focus
|
life sciences
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:scholarships
|
closed-loop system
|
|
gptkbp:seating_capacity
|
500 kg
|
|
gptkbp:status
|
in development
|
|
gptkbp:successor
|
gptkb:Mark_IV_Prototype
|
|
gptkbp:supports
|
mobile launch platform
|
|
gptkbp:sustainability
|
2
|
|
gptkbp:sustainability_initiatives
|
zero waste mission
|
|
gptkbp:upgrades
|
planned
|
|
gptkbp:weight
|
2000 kg
|
|
gptkbp:width
|
5 m
|
|
gptkbp:year
|
2025-12-31
|