Skrobot, Garrett Lee

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JOHN F. KENNEDY SPACE CENTER
ELaNa
Making it Happen!
CalPol~CubeSat Workshop 2012
April 18 - 20
Garrett Skrobot
ELaNa Project Manager
Launch Services Program
NASA
https://ntrs.nasa.gov/search.jsp?R=20120008744 2019-08-30T20:13:04+00:00Z
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JOHN F. KENNEDY SPACE CENTER
CUBESAT
CALIFORNIA POLYTECHNIC STATE UNIVERSITY
JOHN F. KENNEDY SPACE CENTER
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68 Cube elected with 23 Manife ted
JOHN F. KENNEDY SPACE CENTER
Washinglon
Oregon
Wyoming
South Dakota
New Hampshire
Massachusells
South
Carolina
ASA C beSat I it·at·ve
ProposalsJOHN f KENNEDY SPACE CENTER
1st Selection
1st Initiative
2nd Initiative
3rd Initiative
Total
100
60
40
20
# of Props
Submitted
6
16
32
43
97
# of Props
Seleced
4
12
20
32
68
# Manifested
4
10
9
o
23
# Launched
3
5
o
o
8
• 3rd Initiative
• 2nd Initiative
• 1st Initiative
• 1st Selection
O-l£-------------.---------.--------f'
# of Props
Submitted
# of Props
Selected
# Manifested # Launched
6
# of Private
•• •118 ve
# of DoD# of NASA# of Univ
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15t Selection
15t Initiative
2nd Initiative
3rd Initiative
Total
I
4
12
9
20
45
o
o
5
4
9
o
o
6
7
13
o
o
o
2
2
45
40
35
30
25
20
15
10
5
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• 3rd Initiative
• 2nd Initiative
• 15t Initiative
• 15t Selection
# of Univ #of NASA # of 000 # of Private
7
JOHN F. KENNEDY SPACE CENTER
A ACube a
CubeSat
1.5U
Ini ·ative
•Izes
•
1st Selection
1st Initiative
2nd Initiative
I
3rd Initiative
Total
4
7
6
5
23
o
2
4
3
9
o
o
3
4
7
o
4
9
20
33
o
o
o
3
3
35
30
25
20
15
10
5
0
1U 1.5U 2U 3U 6U
• 3rd Initiative
• 2nd Initiative
• 1st Initiative
• 1st Selection
oo
1
1
2
o
6
12
15
33
LEO Non-Sun
Sync
4
o
4
4
12
LEO Sun Sync
ASA Cube a it-ative
CubeSats by Orbit
o
5
3
13
21
51° at 325km
JOHN F. KENNEDY SPACE CENTER
2nd Initiative
3rd Initiative
1st Selection
1st Initiative
35
30
25
20
15
10
5
• 3rd Initiative
• 2nd Initiative
• 1st Initiative
- 1st Selection
0-"'-----------,.-------------..,..-..-------/
51 degree at 325km LEO Sun Sync LEO Non-Sun Sync GTO
JOHN F. KENNEDY SPACE CENTER
A A C be at Carrier
Common
Studied
ABC
In
Development
Aug '12
Common
Studied
2nd Stg
Struts
Section
Flown
Aft End
3rd Stg
Flown
Aft End
Studied
CRS
In
Development
Dec '12
Fairing
Starting
Development
2014
10
JOHN F. KENNEDY SPACE CENTER
Man-fested ission
FY08 FY09 FY10 FY11
March 4th
FY12
August
FY13
June
Feb
FY14
11
JOHN F. KENNEDY SPACE CENTER
FY12 FY13 FY14 FY15 FY16 FY17
Mid 2014
Potent al CRS Fights
2015
12
ano a nche ys e
JOHN F. KENNEDY SPACE CENTER
• During the C beSat Workshop in August 2011,
we talked about the Next og·cal Step for the
aunching of CubeSats
• Our own Nano Launcher System
• So where are we today?
13
450 Km flights
Phase III
,.--_A~_
( Orbital ,
2 Stage system
Large Tanks
Increase Engine
185 Km flights
Phase II - - - -
,.-----IA"---_
( Sub Orbital ,
1 Stage system
Large Tanks
Increase Engine
ana Launcher Syste
> 6 to 12 months>
> 12 to 18 months >
15k to 1OOk feet
flights
JOHN F. KENNEDY SPACE CENTER
Conceptual
Phase I --
_-11,--_......,.
(High Altitude ,
1 Stage system
> 12 to 24 months >~ ..,J
ig AI itude a ncher
JOHN F. KENNEDY SPACE CENTER
• Launch Service Program has placed
Garvey Spacecraft Corporat-on on
contract for a series of high altitude
launches
- Flight 1
» Looking for ridersl
» Launch Date Sept 2012
» Developing a system to el minate P·POD
and attach the CubeSat to the interface
Deck
- Flight 2
» CP9 Mus-StangSat CubeSat system to test
data collect system between two cubesats
• CP9 Mus being developed by CalPoly
• StangSat s a Merritt High School CubeSat
project
- Options for three additional frghts 15
16
cher 81ano a
JOHN F. KENNEDY SPACE CENTER
• Three ASA 2012 Phase I SBIR have been awarded unde
the ano auncher Technology top·c
- Garvey Space
» Alternative Hydrocarbon Propulsion for ano I Micro
Launch Vehicle
• Modify design of flight proven 5K Ibf LOX/ethanol engine ~:===~~
to use propylene Instead
- Interorbital Systems
» Neptune modular rockets for breakthrough low-cost
pace acce s
• A single CP adapted as a rocket, uch a the flight-
ready Interorbital CPMTV, can be used as an ultra low-
cost entry level rocket vehicle for educational program
- Ventions
» A High-Payload Fraction, Pump-Fed, 2-8tage ano
Launch Vehicle
• The proposed nano launch vehicle Is aimed at providing
low-cost and on-demand Insertion of NASA cube- and
nano..ateliites Into LEO as primary payloads
uture - 0 as
JOHN F. KENNEDY SPACE CENTER
• Development of a CubeSat Developers User Guide
• P·POD Power-on System
• Orbital Debris Request for Information
• Six U Carrier System
• ESPA Six U Mount
• Alternative Micro Switch
• RF Gasketing
• Purge System
• CubeSat Propulsion System
17
JOHN F. KENNEDY SPACE CENTER
Clo • 9
Que tions?
18


ELaNA Making it Happen!

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