lux.gif

's type collection


print view : pr_print.gif

Today: 24. Oct 14, visitors total: 10439

please select the headline:

N1-L3 launch vehicle


N1 - Z3
US DoD: SL-15

* Developer:
??
* Payload:
- 1,400 kg to 400 km Orbit
- 700 kg to 1.600 km Orbit

n1lf.gif (2929 Byte)

* Chronology:
- First Launch Date : 02/21/1969
- Last Launch Date : 11/23/1972
- Launches
    Total Number: 4
    Number of Failure: 4
- Success Rate : 0 %
* Launch Vehicle:
- Total Mass: 2,682,650 kg
- Liftoff Thrust: 4,414,909 kgf
- Length with Faring: 105.00 m
- Core Diameter(conical): 16.88 m
- Max. Diameter: 22.33 m

n1lr.gif (26816 Byte)

N1-L3

n1l1.gif (11112 Byte)

* Stage 5: (Block D)
- Engine: RD-58 1D58D
- Number of Engines: 1
- Total Thrust (vac): 8,700 kgf
- Specific Impulse: 348 sec
- Burn Time: 600 sec
- Gross Mass: 17,650 kg
- Empty Mass: 2,650 kg
- Propellants: Kerosene / LOX
- Length: 5.70 m
- Core Diameter: 2.90 m

n1l4.gif (2840 Byte)

*Stage 4: (Block G)
- Engine: NK-19 11D54
- Number of Engines: 1
- Total Thrust (vac): 45,479 kgf
- Specific Impulse: 353 sec
- Burn Time: 443 sec
- Gross Mass: 65,000 kg
- Empty Mass: 7,000 kg
- Propellants: Kerosene / LOX
- Length: 8.90 m
- Core Diameter: 4.40 m

n1l4.gif (2840 Byte)

*Stage 3: (Block V)
- Engine: NK-19 11D53
- Number of Engines: 4
- Total Thrust (vac): 164,000 kgf
- Specific Impulse: 353 sec
- Burn Time: 370 sec
- Gross Mass: 185,000 kg
- Empty Mass: 10,000 kg
- Propellants: Kerosene / LOX
- Length: 12.00 m
- Core Diameter: 4.80 m
- max. Diameter: 7.59 m
- Span of Stubilizer: 6.80 m

n1l3.gif (3872 Byte)

* Stage 2: (Block B)
- Engine: NK-19 11D52
- Number of Engines: 8
- Total Thrust (vac): 1,431,680 kgf
- Specific Impulse: 346 sec
- Burn Time: 120 sec
- Gross Mass: 540,000 kg
- Empty Mass: 35,000 kg
- Propellants: Kerosene / LOX
- Length: 20.00 m
- Core Diameter: 6.80 m
- max. Diameter: 10.30 m
- Span of Stubilizer: 9.80 m

n1l2.gif (5634 Byte)

* Stage 1: (Block A)
- Engine: NK-19 11D51
- Number of Engines: 30
- Total Thrust (vac): 5,130,000 kgf
- Specific Impulse: 330 sec
- Burn Time: 125 sec
- Gross Mass: 1,875,000 kg
- Empty Mass: 125,000 kg
- Propellants: Kerosene / LOX
- Length: 30.00 m
- Core Diameter: 10.00 m
- max. Diameter: 16.88 m
- Span of Stubilizer: 22.33 m

/ back to the top of N1-L3 launch vehicle / Lux's type collection of N1-L3 launch vehicle

 
my sitemap back to my mainsite e-mail me search through my homepage   

Powered by
the Fluid Dynamics Search Engine
v2.0.0.0073 © 2005

  CopyInfo for homepage 1997-2014 by B.Lux, Hamburg - Germany
                    and David Metreveli - Israel.