Vehicle Overview
Note: Payload
performance and estimated cost provided for information only. If you are interested
in contracting for launch services, we recommend that you contact the service provider
directly using the information above.
| |
LEO Payload*
(51.6 deg. inclination) |
GTO Payload*
(7 deg. inclination) |
Estimated Launch Price |
Configuration |
Launch Mass |
| Proton D-1 |
46,000 lb
20,860 kg |
--- |
US $80 - $90 M |
Three Stage Proton Vehicle |
1,475,430 lb
669,130 kg |
| Proton K (D-1-e) |
--- |
9,590 lb
4,350 kg |
US $95 - $105 M |
Three Stage Proton Vehicle
+ Block DM-SL |
1,516,000 lb
687,530 kg |
| Proton M |
--- |
12,125 lb
5,500 kg |
US $95 - $105 M |
Three Stage Proton Vehicle
+ Breeze-M |
1,523,565 lb
691,272 kg |
* Performance from ILS Proton Payload
User's Guide and ILS Web Site.
Vehicle Configuration
| |
Stage 1 |
Stage 2 |
Stage 3 |
Stage 4
(Block DM-SL) |
Stage 4
(Breeze-M) |
| Length |
69.5 ft
21.2 m |
55.9 ft
17.1 m |
13.5 ft
4.1 m |
20.6 ft
6.3 m |
8.6 ft
2.6 m |
| Diameter |
24 ft
7.4 m |
13.4 ft
4.1 m |
13.4 ft
4.1 m |
12.1 ft
3.7 m |
13.1 ft
4.0m |
| Gross Mass |
992,700 lb
450,400 kg |
369,900 lb
167,800 kg |
116,000 lb
52,600 kg |
40,600 lb
18,400 kg |
48,160 lb
21,850 kg |
Propellant
Propellant Mass |
N2O4 / UDMH
924,400 lb
419,400 kg |
N2O4 / UDMH
344,100 lb
156,100 kg |
N2O4 / UDMH
102,600 lb
46,600 kg |
LOX / Syn-Thin
33,180 lb
15,050 kg |
N2O4 / UDMH
43,640 lb
19,800 kg |
Engine**
Thrust
Isp |
RD-253
392,000 lbf
1,745 kN
316 sec |
RD-0210
131,000 lbf
582 kN
326.5 sec |
RD-0210
131,000 lbf
582 kN
326.5 sec |
11D-58M
16,000 lbf
71,000 N
361 sec |
R2000
4,500 lbf
19,620 N
325.5 sec |
| Number of Engines |
6 |
4 |
1 |
1 |
1 |
| Nominal Burn Time |
150 sec |
200 sec |
250 sec |
up to 680 sec |
up to 3,150 sec |
** Note: Vacuum engine performance unless
otherwise specified.
|
