Statements (70)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:academic_programs |
comprised of experienced engineers
|
| gptkbp:application |
launch vehicles
potential for deep space missions |
| gptkbp:budget |
estimated at $100 million for full development
|
| gptkbp:challenges |
overcoming thermal stresses
addressing vibration issues |
| gptkbp:collaboration |
international partnerships
involvement of foreign engineers |
| gptkbp:combustor_type |
staged combustion
|
| gptkbp:competitors |
competes with Space X engines
|
| gptkbp:control_system |
digital control system
|
| gptkbp:cooling_system |
regenerative cooling
|
| gptkbp:design_features |
modular design for easy integration
|
| gptkbp:design_philosophy |
focus on reliability and performance
|
| gptkbp:design_purpose |
high efficiency
|
| gptkbp:designed_by |
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
| gptkbp:development |
gptkb:2000
collaborative team of scientists and engineers |
| gptkbp:development_cost |
estimated at $50 million
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:durability |
not designed for reuse
|
| gptkbp:engine |
staged combustion cycle
|
| gptkbp:engine_type |
gptkb:Team_Rocket
|
| gptkbp:environmental_impact |
lower emissions than previous engines
|
| gptkbp:first_flight |
gptkb:2014
|
| gptkbp:fuel_economy |
high fuel efficiency
|
| gptkbp:fuel_type |
kerosene
|
| gptkbp:funding |
funded by Russian government
|
| gptkbp:future_prospects |
focus on improving efficiency
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-701 rocket engine
|
| gptkbp:improves |
ongoing design improvements
|
| gptkbp:inspired_by |
gptkb:RD-180_engine
|
| gptkbp:invention |
several patents filed
|
| gptkbp:is_tested_for |
gptkb:Moscow
static fire tests conducted at multiple facilities positive results from initial tests GKNPTs im. M. V. Khlopina |
| gptkbp:launch_date |
2025
aims for high launch frequency |
| gptkbp:launch_platform |
gptkb:Russian_space_agency
|
| gptkbp:length |
2.5 m
|
| gptkbp:manufacturer |
gptkb:Khrunichev
|
| gptkbp:material |
advanced composite materials
|
| gptkbp:number_of_rooms |
gptkb:1
10 MPa |
| gptkbp:operational_status |
not yet operational
|
| gptkbp:oxidation_states |
liquid oxygen
|
| gptkbp:part_of |
gptkb:Angara_family_of_rockets
|
| gptkbp:performance |
high thrust-to-weight ratio
|
| gptkbp:project |
delayed due to funding issues
planned upgrades for performance managed by Khrunichev to enhance Russian launch capabilities |
| gptkbp:projected_thrust |
up to 100 k N in future versions
|
| gptkbp:projected_weight |
target weight of 120 kg in future designs
|
| gptkbp:propulsion |
70 k N
45:1 |
| gptkbp:public_interest |
high interest from aerospace community
|
| gptkbp:research_and_development |
ongoing
|
| gptkbp:safety_features |
multiple redundancy systems
|
| gptkbp:specific_impulse |
300 seconds
|
| gptkbp:specification |
available in technical documents
|
| gptkbp:status |
in development
|
| gptkbp:trends |
aligns with trends in reusable rocket technology
|
| gptkbp:used_in |
gptkb:Angara_rocket
|
| gptkbp:weight |
150 kg
|
| gptkbp:bfsParent |
gptkb:Viktor_Mikhailovich_Glushko
|
| gptkbp:bfsLayer |
6
|