RD-0210
Modules

RD-0210

Section Title: Modules
Table Section Text: None

Engine	RD-0203	RD-0204	RD-0206	RD-0208	RD-0209	RD-0210	RD-0211	RD-0213

AKA	8D44	8D44	8D47	8D411	8D412	8D411K	8D412K	8D48

Propulsion Module	RD-0202	RD-0205 (with RD-0207)	RD-0212 (with RD-0214)

Development	1961-1964	1961-1964	1961-1964	1962-1966	1962-1966	1962-1967	1962-1967	1962-1967

Engine Type	Liquid oxidizer rich staged combustion using N2O4/UDMH propellant with an O/F ratio of 2.6

Combustion Chamber Pressure	14.7 MPa (2,130 psi)

Nozzle	Single nozzle (Fixed)	Single nozzle	Single nozzle (Fixed)	Single nozzle with TVC	Single nozzle with TVC	Single nozzle with TVC	Single nozzle with TVC	Single nozzle (Fixed)

Thrust (Vacuum)	559 kN (126,000 lbf)	559 kN (126,000 lbf)	575.5 kN (129,400 lbf)	570 kN (130,000 lbf)	570 kN (130,000 lbf)	582 kN (131,000 lbf)	582 kN (131,000 lbf)	582 kN (131,000 lbf)

Thrust (Sea Level)	500 kN (110,000 lbf)	500 kN (110,000 lbf)

Isp (Vacuum)	311s	311s	326s	326s	326s	326.5s	326.5s	326.5s

Isp(Sea Level)	278s	278s

Burn Time	136s	136s	150s	150s	150s	220s	220s	250s

Length	1.8 m (71 in)	1.8 m (71 in)	2,327 mm (91.6 in)	2,327 mm (91.6 in)	2,327 mm (91.6 in)	2,327 mm (91.6 in)	3,008 mm (118.4 in)

Width	890 mm (35 in)	890 mm (35 in)	1,470 mm (58 in)	1,470 mm (58 in)	1,470 mm (58 in)	1,470 mm (58 in)	1,470 mm (58 in)	1,470 mm (58 in)

Dry Weight	381 kilograms (840 lb)	381 kilograms (840 lb)	540 kilograms (1,190 lb)	540 kilograms (1,190 lb)	566 kilograms (1,248 lb)	566 kilograms (1,248 lb)	550 kilograms (1,210 lb)

Use	UR-200 First Stage	UR-200 First Stage	UR-200 Second Stage	UR-500 Second Stage	UR-500 Second Stage	Proton Second Stage	Proton Second Stage	Proton Third Stage

First Launch	1963-11-06	1963-11-06	1963-11-06	1965-07-16	1965-07-16	1967-03-10	1967-03-10	1967-03-10

Last Launch	1964-10-20	1964-10-20	1964-10-20	1966-07-06	1966-07-06

Status	Retired	Retired	Retired	Retired	Retired	In Production	In Production	In Production

References

Sentence(s)

RD-0212 is a propulsion module comprising one RD-0213 engine.

final_sentence: RD-0212 is a propulsion module comprising one RD-0213 engine.