Modular Propulsion CubeSat Modular Propulsion ... - rocket.com · • High density non-toxic green...
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Modular Propulsion Systems Innovative Propulsion Solutions for CubeSats and SmallSats CubeSat Modular Propulsion Systems • High reliability, high delta-V propulsion for CubeSats and SmallSats • Orbit maintenance, station keeping, and reaction control • High density non-toxic green propellant and traditional hydrazine System Specifications Performance Data la 0174 18 Thrust Range 1U 2U 4U 6U 8U Green (AF-M315E) System Impulse* (N . s) System Dry Mass (kg) System Wet Mass (kg) MPS-130-1U >1,130 1.1 1.7 MPS-130-2U >2,720 1.4 2.8 MPS-135-4U >7,290 3.5 7.2 MPS-135-6U >13,740 4.3 11.2 MPS-135-8U >19,360 5.1 14.7 Hydrazine System Impulse* (N . s) System Dry Mass (kg) System Wet Mass (kg) MPS-120-1U >810 1.2 1.6 MPS-120-2U >1,960 1.5 2.5 MPS-125-4U >5,240 3.6 6.2 MPS-125-6U >9,890 4.4 9.3 MPS-125-8U >13,930 5.1 12.1 ˜ 0.25 – 1.0 N (per thruster) Modular Propulsion System ∆V (m/sec) Modular Propulsion System ∆V (m/sec) *System impulse based on steady state firing operation. Actual total impulse will vary based on operational duty cycles. Total S/C Wet Mass (kg) Total S/C Wet Mass (kg) Piston Tank Systems Pump Tank Systems www.rocket.com
Transcript of Modular Propulsion CubeSat Modular Propulsion ... - rocket.com · • High density non-toxic green...
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Modular PropulsionSystemsInnovative Propulsion Solutionsfor CubeSats and SmallSats
CubeSat Modular Propulsion Systems
• High reliability, high delta-V propulsion for CubeSats and SmallSats
• Orbit maintenance, station keeping, and reaction control
• High density non-toxic green propellant and traditional hydrazine
System Speci�cations
Performance Data
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Thrust Range1U 2U 4U 6U 8U
Green (AF-M315E)
System Impulse* (N.s)
System Dry Mass (kg)
System Wet Mass (kg)
MPS-130-1U
>1,130
1.1
1.7
MPS-130-2U
>2,720
1.4
2.8
MPS-135-4U
>7,290
3.5
7.2
MPS-135-6U
>13,740
4.3
11.2
MPS-135-8U
>19,360
5.1
14.7
Hydrazine
System Impulse* (N.s)
System Dry Mass (kg)
System Wet Mass (kg)
MPS-120-1U
>810
1.2
1.6
MPS-120-2U
>1,960
1.5
2.5
MPS-125-4U
>5,240
3.6
6.2
MPS-125-6U
>9,890
4.4
9.3
MPS-125-8U
>13,930
5.1
12.1
˜0.25 – 1.0 N(per thruster)
Mod
ular
Pro
pul
sion
Sys
tem
∆V (m
/sec
)
Mod
ular
Pro
pul
sion
Sys
tem
∆V (m
/sec
)
*System impulse based on steady state �ring operation. Actual total impulse will vary based on operational duty cycles.
Total S/C Wet Mass (kg) Total S/C Wet Mass (kg)
Piston Tank Systems Pump Tank Systems
www.rocket.com
PDF Output specifications:
Output on an 11 inch by 17 inch page sizeOne sided
In the print menu make sure the following is set:Page Scaling: NoneCheck the box for “Auto-Rotate and Center”
Trim printed sheets at crops, will equal 8 ½ inch x 11 inch
Modular Propulsion SystemsInnovative Propulsion Solutions for CubeSats and SmallSats
• High reliability, high delta-V propulsion for CubeSats and SmallSats
• Orbit maintenance, station keeping, and reaction control
• High density non-toxic green propellant and traditional hydrazine
Size of Propulsion System1U = ~10 x 10 x 10 cm volume
2U = ~10 x 10 x 20 cm volume
4U = ~22 x 20 x 10 cm volume
6U = ~22 x 20 x 16 cm volume
8U = ~22 x 20 x 22 cm volume
(U Designations for CubeSat systems only)
Model Number Designator0 = Piston fed with condensable pressurant
5 = Pump fed with PMD tanks
Propellant Type1 = Cold gas
2 = Hydrazine (most requested)3 = ‘Green’ AF-M315E (most requested)4 = Electric Propulsion
System Size Class1 = CubeSat systems (most requested)2 = SmallSat systems
3 = ESPA Ring systems
System ClassMPS = Modular Propulsion System
Figure Models
MPS-130-1UMPS-120-1U
MPS-130-2UMPS-120-2U
MPS-135-4UMPS-125-4U
MPS-135-6UMPS-125-6U
MPS-135-8UMPS-125-8UC
ub
eSat
Mo
dula
r P
rop
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ion S
yste
m C
on�g
ura
tio
ns
Propulsion System Designations:
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MPS – 1 3 5 – 6U
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