Soviet Bloc
31-12-2003, 06:18
The ARSB announced today that it plans to begin a grand space program by first building two space stations (each with four modules) named Groza I and Groza II. After this initial deployment the stations will be manned with minimum crews replenished by 'Progress'-type Soyuz modules. The crew will be replaced every 6-8 months. The twin stations will house up to four people each and have three docking ports. This project will prove to be very expensive, although our budget should handle it over the years that it would take to implement. Any help would be appreciated.
Stats for Groza-type stations:
Pods-4 (one living quarters, one scientific, one utility[with life support systems, storage, etc.], one docking with small gym on end)
Crew- Min.:2 Max.:4
Power- eight 450 sq. ft. solar panels providing bulk of power with onboard emergency batteries and hydrogen fuel cells.
Systems- Oxygen generators, emergency oxygen cells, air recycling unit, water recycling unit, ALMRS/TTAC-09 SV targetting, tracking and acquisition system, advanced satellite/radio communications system (linked with all stations).
Placement: located along equator on opposite ends of planet
After the two Groza-type stations are built, four smaller SA3O-type stations will be built. They will be staffed with minimum crews that will be replaced every 6-8 months.
SA30-type station spefications-
Pods- 2 (one living quarters, one utility) with small docking module on one end (with four docking ports)
Crew- Min:2 Max:3
Power- four 250 sq. ft. solar panels for bulk of power, onboard emergency batteries and hydrogen fuel cells.
Systems- Oxygen generators, emergency oxygen cells, air recycling unit, water recycling unit, ALMRS/TTAC-09 SV targetting, tracking and acquisition system, advanced satellite/radio communications system (linked with all stations).
Positions: Located in positions that would equal out to be equal coverage of planet
*Note- THese stations have no weapons on them whatsoever*
After these stations are completed, 12 rockets will be launched (each having a single Soyuz A3 space interceptor on board). Two Soyuz A3s will be docked at each station automatically using ground-based controlling. (The onboard crew at each station would be the crew of the Soyuz units except one which would stay behind)
Soyuz A3 Space Interceptor
Note: The Soyuz A3 can also be easily configured to be operated by a single cosmonaut (for piloting and combat reasons).
Performance: Soyuz A3 can accommodate a crew of two and 50 kg cargo.
Principal units: forward Weapons Module, center Crew Module, and aft Service Module
Overall length: 6.98 m with docking probe withdrawn
Habitable volume: ~10 m3
Launch mass: 7,070 kg
Landing mass: about 3,000 kg
Thermal protection: Soyuz-TM's exterior, apart from the SM radiators, is protected by green thermal blanketing; the CM carries eight blankets held by apex + base rings released when the other modules separates. Information on the CM's current re-entry protection is not available
Life support systems: Soyuz A3 is hermetically sealed on the pad under sea level conditions and its 184-263 mbar partial O2 pressure maintained by regeneration through potassium superoxide and LiOH cylinders. The bulk of the system is housed in the WM but the CM carries a smaller, independent unit. O2 bottles provide emergency protection.The cosmonauts wear pressure suits. Also, oxygen is produced as a byproduct of the hydrogen fuel cells (When engaged).
Avionics/control: SB-ASCCS-2- Allows for ground-based control via satellite link, radio transmission, or any other transmission type. Also allows optical flight capabilities by the commander/crew of the craft by utilizing numerous sensors, fiber-optic cables, advanced telemtric computers, and an integrated SB-ASD display system with 5 different screens and twin joysticks (one being vertical [up, down] thrust and the other being horizontal [forward, backward, sides] thrust) and a single variable throttle for the main engine.
CREW MODULE
The crew module carries a single 70 cm diameter overhead hatch, opened from either side, and two 70 cm diameter side hatches for the primary/reserve parachute systems. The CM provides occupants with two 20 cm diameter portholes, one either side of the control panels.
Crew size: 2 (alternately, a 100 kg cargo pod can replace one crewmember or ammunition storage)
Length: 2.2 m
Maximum diameter: 2.2 m
Habitable volume: ~4 m3
Total mass: 2,850 kg
Attitude & orbit control system
thrusters: 6 x 67 N (activated for reentry only)
propellant: H2O2
L/D hypersonic: 0.25-0.30
Power: SB-AHFC system (Advanced hydrogen fuel cell system) with a back-up small battery
Landing system: On a normal mission, descent is initiated by a 3-4 min ~155 m/s retroburn by the main engine, followed by WM and then SM ejection. The landing system is activated by pressure switch at 9-11 km and 850 km/h, with two sequential stabilizing drogues releasing the 4.25 m braking 'chute from the port compartment. The primary canopy is deployed reefed at 8 km. It is freed to its full 35.5 m diameter at a descent rate of around 35 m/s to reduce sink rate to 8 m/s. The reserve systems yields 10 m/s descent rate with 25 m 'chute, activated at 6 km. The heat shield is dropped at about 3 km some 5 min before landing to clear the base retromotors for a soft landing. Four solids are triggered by a radar altimeter about 2 m above the ground to cushion the impact. Touchdown is normally on land but Soyuz is equipped for water landings
WEAPONS MODULE
The spherodial Weapons module (WM) provides space for cargo, food, waste management services, orbital experimentation on solo missions and EVA operations through the 65 cm diameter side hatch. The forward 80 cm hatch houses the docking apparatus inside a 1.3 m diameter docking collar and connections for electrical, communications and hydraulic links. The Weapons module is primarily used for combat and contains the ALMRS/TTAC-09 SV tracking and targetting system which tracks up to 560 targets and can track them indefinetely. The Weapons module also contains a large forward window (triple-layered treated glass with finishing layers of fiber-reinforced plexiglass) that can be covered by a variable steel plate (with ceramics and DU armor) that can be securely fastened to interior or exterior. For targetting units the WM has 8 variable monitors (one large one for a forward view, 5 smaller ones for other views and two for weapons statistics and targetted units' statistics). When the gunner-control system is engaged, the gunner operates the craft using twin joysticks that operate the vertical and horizontal axis' of the unit while the pilot operates throttle and back-up control. On the vertical axis joystick is two buttons (one on top and one where index finger should be), the index-finger button operates the main gun and the top button operates the launcher for the Kestril Mk. II space missile (which can target units automatically or track a certain target).
Length: 3.0 m
Maximum diameter: 2.2 m
Habitable volume: ~6 m3
Total mass: 1,200 kg
Other: The WeaponsModule contains twin SIC-10 rail-type cannons which can fire iron-encased depleted uranium slugs using power collected by solar panels or the onboard advanced hydrogen fuel cell stack (roughly eight cells).
SERVICE MODULE
The service module (SM) supports the CM on its forward face. A 45 cm deep pressurized section houses hydrogen fuel cells, power conditioning systems for the twin solar panels, batteries and control systems. Umbilicals link this section with the CM's base panel. The unpressurized rear section holds the propulsion system and its four spherical containers; the outer surface provides a mounting for ~8 m2 of thermal radiators.
Length: 2.3 m
Diameter: 2.2 m (flaring to 2.7 m at aft end)
Total mass: 2,700 kg Soyuz / 2,750 kg Soyuz-T / 2,950 kg Soyuz-TM
Power: Soyuz A3 introduced twin 4-segment solar wings 1.4 x 4.4 m feeding batteries in the service module. Output ~1.3 kW, with a significant proportion lost in cabling/processing. TM span 10.6 m. Soyuz locks on to the Sun with a sensor and slowly cartwheels around the Sun axis when in standby mode (non-combat), energy is stored in onboard batteries.
Other: The SM contains four small 'bays', each housing a single Kestril Mk. II space missile.
*I can provide any specs for the Kestril Mk. IIs or the SIC-10 rail gun. Also, the ARSB is looking for new engines to place on the Soyuz A3s*
(Comments, questions?)
Stats for Groza-type stations:
Pods-4 (one living quarters, one scientific, one utility[with life support systems, storage, etc.], one docking with small gym on end)
Crew- Min.:2 Max.:4
Power- eight 450 sq. ft. solar panels providing bulk of power with onboard emergency batteries and hydrogen fuel cells.
Systems- Oxygen generators, emergency oxygen cells, air recycling unit, water recycling unit, ALMRS/TTAC-09 SV targetting, tracking and acquisition system, advanced satellite/radio communications system (linked with all stations).
Placement: located along equator on opposite ends of planet
After the two Groza-type stations are built, four smaller SA3O-type stations will be built. They will be staffed with minimum crews that will be replaced every 6-8 months.
SA30-type station spefications-
Pods- 2 (one living quarters, one utility) with small docking module on one end (with four docking ports)
Crew- Min:2 Max:3
Power- four 250 sq. ft. solar panels for bulk of power, onboard emergency batteries and hydrogen fuel cells.
Systems- Oxygen generators, emergency oxygen cells, air recycling unit, water recycling unit, ALMRS/TTAC-09 SV targetting, tracking and acquisition system, advanced satellite/radio communications system (linked with all stations).
Positions: Located in positions that would equal out to be equal coverage of planet
*Note- THese stations have no weapons on them whatsoever*
After these stations are completed, 12 rockets will be launched (each having a single Soyuz A3 space interceptor on board). Two Soyuz A3s will be docked at each station automatically using ground-based controlling. (The onboard crew at each station would be the crew of the Soyuz units except one which would stay behind)
Soyuz A3 Space Interceptor
Note: The Soyuz A3 can also be easily configured to be operated by a single cosmonaut (for piloting and combat reasons).
Performance: Soyuz A3 can accommodate a crew of two and 50 kg cargo.
Principal units: forward Weapons Module, center Crew Module, and aft Service Module
Overall length: 6.98 m with docking probe withdrawn
Habitable volume: ~10 m3
Launch mass: 7,070 kg
Landing mass: about 3,000 kg
Thermal protection: Soyuz-TM's exterior, apart from the SM radiators, is protected by green thermal blanketing; the CM carries eight blankets held by apex + base rings released when the other modules separates. Information on the CM's current re-entry protection is not available
Life support systems: Soyuz A3 is hermetically sealed on the pad under sea level conditions and its 184-263 mbar partial O2 pressure maintained by regeneration through potassium superoxide and LiOH cylinders. The bulk of the system is housed in the WM but the CM carries a smaller, independent unit. O2 bottles provide emergency protection.The cosmonauts wear pressure suits. Also, oxygen is produced as a byproduct of the hydrogen fuel cells (When engaged).
Avionics/control: SB-ASCCS-2- Allows for ground-based control via satellite link, radio transmission, or any other transmission type. Also allows optical flight capabilities by the commander/crew of the craft by utilizing numerous sensors, fiber-optic cables, advanced telemtric computers, and an integrated SB-ASD display system with 5 different screens and twin joysticks (one being vertical [up, down] thrust and the other being horizontal [forward, backward, sides] thrust) and a single variable throttle for the main engine.
CREW MODULE
The crew module carries a single 70 cm diameter overhead hatch, opened from either side, and two 70 cm diameter side hatches for the primary/reserve parachute systems. The CM provides occupants with two 20 cm diameter portholes, one either side of the control panels.
Crew size: 2 (alternately, a 100 kg cargo pod can replace one crewmember or ammunition storage)
Length: 2.2 m
Maximum diameter: 2.2 m
Habitable volume: ~4 m3
Total mass: 2,850 kg
Attitude & orbit control system
thrusters: 6 x 67 N (activated for reentry only)
propellant: H2O2
L/D hypersonic: 0.25-0.30
Power: SB-AHFC system (Advanced hydrogen fuel cell system) with a back-up small battery
Landing system: On a normal mission, descent is initiated by a 3-4 min ~155 m/s retroburn by the main engine, followed by WM and then SM ejection. The landing system is activated by pressure switch at 9-11 km and 850 km/h, with two sequential stabilizing drogues releasing the 4.25 m braking 'chute from the port compartment. The primary canopy is deployed reefed at 8 km. It is freed to its full 35.5 m diameter at a descent rate of around 35 m/s to reduce sink rate to 8 m/s. The reserve systems yields 10 m/s descent rate with 25 m 'chute, activated at 6 km. The heat shield is dropped at about 3 km some 5 min before landing to clear the base retromotors for a soft landing. Four solids are triggered by a radar altimeter about 2 m above the ground to cushion the impact. Touchdown is normally on land but Soyuz is equipped for water landings
WEAPONS MODULE
The spherodial Weapons module (WM) provides space for cargo, food, waste management services, orbital experimentation on solo missions and EVA operations through the 65 cm diameter side hatch. The forward 80 cm hatch houses the docking apparatus inside a 1.3 m diameter docking collar and connections for electrical, communications and hydraulic links. The Weapons module is primarily used for combat and contains the ALMRS/TTAC-09 SV tracking and targetting system which tracks up to 560 targets and can track them indefinetely. The Weapons module also contains a large forward window (triple-layered treated glass with finishing layers of fiber-reinforced plexiglass) that can be covered by a variable steel plate (with ceramics and DU armor) that can be securely fastened to interior or exterior. For targetting units the WM has 8 variable monitors (one large one for a forward view, 5 smaller ones for other views and two for weapons statistics and targetted units' statistics). When the gunner-control system is engaged, the gunner operates the craft using twin joysticks that operate the vertical and horizontal axis' of the unit while the pilot operates throttle and back-up control. On the vertical axis joystick is two buttons (one on top and one where index finger should be), the index-finger button operates the main gun and the top button operates the launcher for the Kestril Mk. II space missile (which can target units automatically or track a certain target).
Length: 3.0 m
Maximum diameter: 2.2 m
Habitable volume: ~6 m3
Total mass: 1,200 kg
Other: The WeaponsModule contains twin SIC-10 rail-type cannons which can fire iron-encased depleted uranium slugs using power collected by solar panels or the onboard advanced hydrogen fuel cell stack (roughly eight cells).
SERVICE MODULE
The service module (SM) supports the CM on its forward face. A 45 cm deep pressurized section houses hydrogen fuel cells, power conditioning systems for the twin solar panels, batteries and control systems. Umbilicals link this section with the CM's base panel. The unpressurized rear section holds the propulsion system and its four spherical containers; the outer surface provides a mounting for ~8 m2 of thermal radiators.
Length: 2.3 m
Diameter: 2.2 m (flaring to 2.7 m at aft end)
Total mass: 2,700 kg Soyuz / 2,750 kg Soyuz-T / 2,950 kg Soyuz-TM
Power: Soyuz A3 introduced twin 4-segment solar wings 1.4 x 4.4 m feeding batteries in the service module. Output ~1.3 kW, with a significant proportion lost in cabling/processing. TM span 10.6 m. Soyuz locks on to the Sun with a sensor and slowly cartwheels around the Sun axis when in standby mode (non-combat), energy is stored in onboard batteries.
Other: The SM contains four small 'bays', each housing a single Kestril Mk. II space missile.
*I can provide any specs for the Kestril Mk. IIs or the SIC-10 rail gun. Also, the ARSB is looking for new engines to place on the Soyuz A3s*
(Comments, questions?)