Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:can_be_used_in |
satellite propulsion
|
| gptkbp:conducts_research_on |
sustainable space exploration
electric propulsion advancements |
| gptkbp:developed_by |
gptkb:Ad_Astra_Rocket_Company
private funding |
| gptkbp:enhances |
mission flexibility
|
| gptkbp:has_achieved |
thrust levels up to 5 Newtons
|
| gptkbp:has_applications_in |
deep space missions
|
| gptkbp:has_cooling_requirements |
gptkb:hydroelectric_power_generation
|
| gptkbp:has_development_support_from |
gptkb:NASA
|
| gptkbp:has_potential_to_enable |
interplanetary travel
|
| gptkbp:has_potential_to_reduce |
travel time to Mars
|
| gptkbp:has_version |
including VX-200 and VX-100
|
| https://www.w3.org/2000/01/rdf-schema#label |
VASIMR engine
|
| gptkbp:is_aimed_at |
reducing mission costs
|
| gptkbp:is_aresearch_project_of |
gptkb:Ad_Astra_Rocket_Company
|
| gptkbp:is_based_on |
magnetoplasma dynamics
|
| gptkbp:is_capable_of |
variable thrust levels
|
| gptkbp:is_considered |
gptkb:Mars_missions
deep space exploration missions satellite station-keeping future crewed missions to asteroids |
| gptkbp:is_considered_innovative_for |
its efficiency and versatility
|
| gptkbp:is_designed_for |
long-duration space missions
|
| gptkbp:is_developed_to_improve |
spacecraft maneuverability
|
| gptkbp:is_developed_with_focus_on |
reusability
|
| gptkbp:is_evaluated_by |
gptkb:human_spaceflight
space agencies worldwide its scalability its environmental impact commercial spaceflight applications |
| gptkbp:is_influenced_by |
previous ion propulsion technologies
|
| gptkbp:is_part_of |
NASA's Artemis program considerations
NASA's advanced propulsion program advanced propulsion systems research the evolution of propulsion technologies. the future of space exploration technology |
| gptkbp:is_supported_by |
various aerospace organizations
|
| gptkbp:is_tested_for |
gptkb:International_Space_Station
performance metrics vacuum chambers various space environments different propellant types |
| gptkbp:is_used_for |
space propulsion
|
| gptkbp:is_used_in |
future lunar missions
|
| gptkbp:operates |
ionized gas
|
| gptkbp:operational_use |
high specific impulse
|
| gptkbp:provides_support_for |
human exploration of Mars
|
| gptkbp:uses |
gptkb:plasma
|
| gptkbp:uses_magnetic_fields |
to contain plasma
|
| gptkbp:was_a_demonstration_of |
plasma flow control
|
| gptkbp:was_first_tested_in |
gptkb:2000
|
| gptkbp:bfsParent |
gptkb:Ad_Astra_Rocket_Company
|
| gptkbp:bfsLayer |
5
|