GSR plane's mains characteristics

Characteristic	Value
Wings's surface, m²	240
Wings's length, m	16.875
Wing's depth along the plane's axe, m	32.6
Depth's stabilizers, m	4.5
Wing shaped's thickness, leading edge/end	0.025/0.03
Elevons's surface, m²	24
Wingspan, m	16.5
Length of the vertical stabilizers, m	4.5
Lengthening of the wing, m	1.14
Elevon's wingspan, m	10.2
Wing's inclinaison (start/end), °	80 / 60
Length of the fuselage, m	38
Maximum diameter of the fuselage, m	4.15
Front surface of the fuselage (engines included), m²	20.9
Engine's intack surface, m²	12.8
Engine span, m	6.2
Rudder's surface, m²	2 x 18.5

Auxiliary rocket's mains characteristics

1st stage
Characteristics	Variants
	Main	Secondary
Specific impulse, s	460	455
Length (with the cover), m	27.75	28.71
Empty mass, kg	6150	8620
Thrust on the ground (without the orbital space-plane), kgf	52700	51120
Componants ratio	1:14	1:7.5
Empty masse, kg	5500	7700
Lift off mass, kg	47500	45950
Fuel	Liquide hygrogen	Liquide hygrogen
Mass, kg	2800	4500
Volume, m³	40	60
Oxidizer	Liquid fluorine	Liquid oxygen
Masse, kg	39200	33750
Volume, m³	25	30.9
Tank's diameter, m	2.5	3.0
GRS thrust, kgf	4 x 25000	4 x 25000
2nd stage
Empty masse, kg	650	920
PLift off mass (without the orbital plane), kg	5200	5170
Fuel	Liquid hydrogen	Liquid hydrogen
Mass, kg	310	500
Volume, m³	4.42	6.67
Oxidizer	Liquid fluorine	Liquid oxygen
Mass, kg	4240	3750
Volume, m³	2.7	3.43
GRD's thrust, kgf	1 x 25000	1 x 25000