CanSat 2025 Critical Design Review (CDR) Presentation Outline
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CDR: Team ### (Team Number and Name)
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CDR: Team ### (Team Number and Name)
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CDR: Team ### (Team Number and Name)
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CanSat 2025
CDR: Team ### (Team Number and Name)
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Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
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The purpose of this section is to introduce the reviewer to the overall requirements
and configuration of the CanSat. This provides a basis for the details presented in
the subsystem sections.
CanSat 2025
C
DR: Team ### (Team Number and Name)
6
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CanSat 2025 CDR
: Team ### (Team Number and Name)
7
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CanSat 2025
C
DR: Team ### (Team Number and Name)
8
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
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Pre-launch activities
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Launch and descent operations
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Post-launch recovery and data reduction
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Absolutely no hand-drawn diagrams
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Photos are acceptable
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
10
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–
Dimensions
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Placement of major components
•
Sensors, electronics, radio, power, mechanisms
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Relevant configurations
•
P
ayload, launch configuration, deployed, etc.
CanSat 2025 CDR
: Team ### (Team Number and Name)
11
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Focus on launch configuration
–
Include all descent control apparatus (no sharp protrusions)
–
What is the clearance? (Leave margin to allow
easy
deployment!)
•
N
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:
–
In past years there were a large number of CanSats that did not
deploy from the payload sections of the rocket because of
protrusions or because the CanSat was too wide to fit in the rocket
–
Lack of sharp protrusions and fit within the Launch Vehicle will also
be scored at the Flight Readiness Review
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
12
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CanSat 2025 CDR
: Team ### (Team Number and Name)
13
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–
Include brief discussion of what the sensors are used for
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Include rationale
–
Clearly explain why changes were made, including
things like:
•
Power limitations
•
Testing
•
Component size
•
Availability
CanSat 2025 CDR
: Team ### (Team Number and Name)
14
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
15
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–
Sensor accuracy and data format
–
Overview of data processing (including equations, as
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–
If there is no sensor, have a page that states it to receive
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Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
16
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Sensor accuracy and data format
–
Overview of data processing (including equations, as
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–
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the points
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
17
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Overview of data processing (including equations, as
appropriate)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
18
P
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:
–
Sensor accuracy and data format
–
Overview of data formats (including equations, as
appropriate)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
19
A
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:
–
Sensor accuracy and data format
–
Overview of data formats (including equations, as
appropriate)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
20
P
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I
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:
–
Sensor accuracy and data format
–
Overview of data formats (including equations, as
appropriate)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
21
G
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I
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:
–
Ensure your camera meets the requirement of 640x480
pixels in color
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
22
P
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I
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:
–
Ensure your camera meets the requirement of 640x480
pixels in color
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
23
D
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CanSat 2025 CDR
: Team ### (Team Number and Name)
24
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Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
25
D
e
s
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C
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Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
26
C
o
n
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P
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D
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c
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t
c
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t
r
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l
h
a
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d
w
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e
–
Include details on parachute design
•
Shape selection
•
Size selection
•
color
•
etc
•
T
h
i
s
d
i
s
c
u
s
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y
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
27
A
u
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o
-
g
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D
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s
c
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C
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•
D
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.
–
shape
–
size
–
expected rotation rate
–
aerodynamics
Presenter: Name goes here
A
u
t
o
-
g
y
r
o
D
e
s
c
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n
t
S
t
a
b
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C
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D
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D
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d
n
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t
u
m
b
l
e
–
Describe mechanisms used
–
Describe how payload is kept nadir pointing
–
Show design of method
–
Active or passive stability control
28
CanSat 2025 CDR
: Team ### (Team Number and Name)
28
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
29
D
e
s
c
e
n
t
R
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E
s
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P
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C
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S
a
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c
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f
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s
–
Parachute
–
Auto-gyro
•
I
n
c
l
u
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e
d
i
s
c
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s
i
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f
–
Calculations used
–
Assumptions
•
T
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•
L
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M
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d
.
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
30
M
e
c
h
a
n
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c
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S
u
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y
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D
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N
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(
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)
G
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CanSat 2025 CDR
: Team ### (Team Number and Name)
31
M
e
c
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–
Include overview of major structural elements, material
selection, and interface definitions
31
Presenter: Name goes here
M
e
c
h
a
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i
c
a
l
S
u
b
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C
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H
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i
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s
CanSat 2025 CDR
: Team ### (Team Number and Name)
32
CanSat 2025 CDR
: Team ### (Team Number and Name)
32
Presenter: Name goes here
C
a
n
s
a
t
M
e
c
h
a
n
i
c
a
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L
a
y
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•
S
h
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w
s
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c
t
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(
C
A
D
m
o
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l
)
–
include dimension drawings
•
I
d
e
n
t
i
f
y
l
o
c
a
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i
o
n
o
f
e
l
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p
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•
I
d
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a
j
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c
h
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n
i
c
a
l
p
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s
–
mechanisms such as springs, hinges, etc.
•
S
t
r
u
c
t
u
r
a
l
m
a
t
e
r
i
a
l
s
e
l
e
c
t
i
o
n
(
s
)
CanSat 2025 CDR
: Team ### (Team Number and Name)
33
Presenter: Name goes here
C
o
n
t
a
i
n
e
r
D
e
s
i
g
n
•
S
h
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w
a
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x
p
l
a
i
n
c
o
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t
a
i
n
e
r
d
e
s
i
g
n
.
–
Show any changes from reference design
–
Show dimensions including required dimensions
–
How is shoulder dimensions verified for proper fit
34
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
P
a
y
l
o
a
d
P
r
e
-
D
e
p
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C
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f
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i
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•
S
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p
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y
e
d
c
o
n
f
i
g
u
r
a
t
i
o
n
–
Explain how payload is secured in container.
35
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
P
a
y
l
o
a
d
R
e
l
e
a
s
e
•
S
h
o
w
a
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d
e
x
p
l
a
i
n
h
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w
p
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e
a
s
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d
f
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m
c
o
n
t
a
i
n
e
r
.
–
Mechanisms used for release
–
Sequence of operation for release
–
Trigger for release
36
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
P
a
y
l
o
a
d
D
e
p
l
o
y
m
e
n
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C
o
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f
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i
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n
•
S
h
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w
a
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d
e
x
p
l
a
i
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a
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y
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c
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m
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a
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d
/
o
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s
t
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a
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c
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n
g
e
o
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o
p
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n
w
h
e
n
p
a
y
l
o
a
d
i
s
r
e
l
e
a
s
e
d
.
–
Not the auto-gyro.
–
If none, state no change in payload structure
37
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
CanSat 2025 PDR:
Team ### (Team Number and Name)
38
A
u
t
o
-
g
y
r
o
d
e
p
l
o
y
m
e
n
t
•
S
h
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w
a
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d
e
x
p
l
a
i
n
h
o
w
a
u
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o
-
g
y
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o
m
e
c
h
a
n
i
s
m
i
s
d
e
p
l
o
y
e
d
.
–
Show mechanisms
–
Sequence of deployment
Presenter: Name goes here
G
r
o
u
n
d
C
a
m
e
r
a
P
o
i
n
t
i
n
g
•
S
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x
p
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a
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h
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t
s
n
o
r
t
h
d
u
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i
n
g
d
e
s
c
e
n
t
–
Show mechanisms
–
Explain operations
–
Pointing algorithms if any
39
S
t
r
u
c
t
u
r
e
S
u
r
v
i
v
a
b
i
l
i
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•
A
s
a
p
p
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c
a
b
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f
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C
a
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s
a
t
,
d
i
s
c
u
s
s
:
–
Electronic component mounting methods
–
Electronic component enclosures
–
Acceleration and shock force requirements and testing
–
Securing electrical connections (glue, tape, etc.)
•
Consider required judge verification during pre-flight check in
–
Descent control attachments
CanSat 2025 CDR
: Team ### (Team Number and Name)
40
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
41
M
a
s
s
B
u
d
g
e
t
•
T
a
b
l
e
(
s
)
p
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o
v
i
d
i
n
g
t
h
e
f
o
l
l
o
w
i
n
g
:
–
Mass of each component of the Cansat
–
Mass of each structural element
–
Sources/uncertainties – whether the masses are
estimates, from data sheets, measured values, etc.
–
Total mass of all components and structural elements
–
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CanSat 2025 CDR
: Team ### (Team Number and Name)
42
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CanSat 2025 CDR
: Team ### (Team Number and Name)
43
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CanSat 2025 CDR
: Team ### (Team Number and Name)
43
Presenter: Name goes here
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CanSat 2025 CDR
: Team ### (Team Number and Name)
44
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
45
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clock with independent power supply
–
Reset tolerance
–
Real time clock should have independent battery backup
to maintain time through power transients
CanSat 2025
C
DR: Team ### (Team Number and Name)
46
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
47
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–
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–
Mass
CanSat 2025 CDR
: Team ### (Team Number and Name)
47
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
48
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How is this managed during each mission phase?
•
N
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:
–
Communications failures have occurred often over the past several
years of the competition
–
You are encouraged to use your radios in all of your development
and testing to better ensure mission success
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Ideally you have started working with the radio and communications
protocol
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CanSat 2025 CDR
: Team ### (Team Number and Name)
49
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–
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with complete descriptions
–
Does the presented format match the Competition Guide
requirements?
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
50
P
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with complete descriptions
–
Does the presented format match the Competition Guide
requirements?
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
51
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CanSat 2025 CDR
: Team ### (Team Number and Name)
52
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CanSat 2025 CDR
: Team ### (Team Number and Name)
53
CanSat 2025 CDR
: Team ### (Team Number and Name)
53
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
54
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–
Include all major components
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–
Voltages
–
Current capacity
–
How much current battery can generate instantly
–
How many batteries
–
How are they connected if more than one battery
CanSat 2025
C
DR: Team ### (Team Number and Name)
55
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
56
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–
Power consumption (Wh) of all components
–
Expected duty cycles for all components
–
Source/uncertainty for each line item
•
Estimate, data sheet, measurement, etc.
–
Total power consumed (Wh)
–
Power sources and total power available
–
Margin : Difference of battery watt hours versus payload
power consumption in watt hours
•
Requirement defined in mission guide states that the payload
must be powered for at least two hours
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
57
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CanSat 2025 CDR
: Team ### (Team Number and Name)
58
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Programming languages
–
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–
Brief summary of the FSW tasks
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CanSat 2025 CDR
: Team ### (Team Number and Name)
59
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
60
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–
Sampling of sensors (including rates)
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Communications (command and telemetry)
–
Data storage (if applicable)
–
Mechanism activations
–
Major decision points in the logic
•
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61
CanSat 2025 CDR:
Team ### (Team Number and Name)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
62
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•
I
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c
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:
–
Prototyping and prototyping environments
–
Software subsystem development sequence
–
Development team
–
Test methodology
•
D
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P
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Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
63
G
r
o
u
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(
G
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(
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CanSat 2025 CDR
: Team ### (Team Number and Name)
64
G
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•
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.
CanSat 2025 CDR
: Team ### (Team Number and Name)
65
Presenter: Name goes here
G
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h
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What components and how they connect
•
S
p
e
c
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f
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i
o
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s
–
How long ground station can operate on battery
–
Overheating mitigation (how do you keep laptop from
getting so hot, it stops operating? Remember, it will be
hot and the ground station will be in the open sun.)
–
Auto update mitigation (how do you keep the OS from
starting an update during operations? It has happened
before with Windows OS)
66
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
67
G
C
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A
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t
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c
l
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e
:
–
Antenna construction, portability, and coverage
•
Diagram is recommended
–
Antenna compliance with hand-held requirement
–
Distance link predictions and margins
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
G
C
S
S
o
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How will Telemetry be displayed in real time and how will
it be recorded?
•
C
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S
i
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–
Describe how the ground system reads the profile and
transmits simulation commands
•
P
r
o
g
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s
s
s
i
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c
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P
D
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CanSat 2025 CDR
: Team ### (Team Number and Name)
68
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
69
C
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I
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(
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G
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CanSat 2025 CDR
: Team ### (Team Number and Name)
70
C
a
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S
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Presenter: Name goes here
•
D
i
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P
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D
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e
m
–
Sensors
–
CDH
–
EPS
–
Radio communications
–
FSW
–
Mechanical
–
Descent Control
71
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
I
n
t
e
g
r
a
t
e
d
L
e
v
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F
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i
s
b
u
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t
–
Descent testing
–
Communications
–
Mechanisms
–
Deployment
–
Simulation
72
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
E
n
v
i
r
o
n
m
e
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t
a
l
T
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a
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t
e
s
t
i
n
g
–
Drop test
–
Thermal test
–
Vibration test
–
Fit Check
–
Vacuum test
73
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
T
e
s
t
P
r
o
c
e
d
u
r
e
s
D
e
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74
•
F
o
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a
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A
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M
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b
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c
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a
r
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
Presenter: Name goes here
S
i
m
u
l
a
t
i
o
n
T
e
s
t
P
l
a
n
•
D
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f
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i
m
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l
a
t
i
o
n
t
e
s
t
i
n
g
–
What parts of the cansat get tested during simulation
–
How is the simulation implemented
75
CanSat 2025 CDR:
Team ### (Team Number and Name)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
76
M
i
s
s
i
o
n
O
p
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r
a
t
i
o
n
s
&
A
n
a
l
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s
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s
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n
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r
N
a
m
e
(
s
)
G
o
H
e
r
e
CanSat 2025 CDR
: Team ### (Team Number and Name)
77
O
v
e
r
v
i
e
w
o
f
M
i
s
s
i
o
n
S
e
q
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f
E
v
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t
s
•
L
a
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c
h
-
d
a
y
s
e
q
u
e
n
c
e
o
f
e
v
e
n
t
s
–
Should start with arrival at the launch site and proceed
through recovery and data analysis
•
I
n
c
l
u
d
e
:
–
Flowchart of events
–
Team member roles and responsibilities
–
Antenna construction and ground system setup
–
CanSat assembly and test
–
Delivery of telemetry data file to field judge for review
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
78
F
i
e
l
d
S
a
f
e
t
y
R
u
l
e
s
C
o
m
p
l
i
a
n
c
e
•
D
i
s
c
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d
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v
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d
c
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M
i
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s
i
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s
O
p
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r
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o
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s
M
a
n
u
a
l
f
o
r
y
o
u
r
C
a
n
S
a
t
–
T
he Mission Operations Manual
is
due at the Flight
Readiness Review the day before launch
•
Assemble in three ring binder (the launch site may be windy)
•
D
i
s
c
u
s
s
d
e
v
e
l
o
p
m
e
n
t
s
t
a
t
u
s
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
79
C
a
n
S
a
t
L
o
c
a
t
i
o
n
a
n
d
R
e
c
o
v
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r
y
•
D
i
s
c
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s
s
h
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y
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f
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d
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o
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r
C
a
n
S
a
t
s
i
n
t
h
e
f
i
e
l
d
–
Discuss Cansat recovery
–
Color selection of visible components
–
CanSat return address labeling
Presenter: Name goes here
M
i
s
s
i
o
n
R
e
h
e
a
r
s
a
l
A
c
t
i
v
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s
•
D
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s
i
n
c
l
u
d
i
n
g
:
–
Details of activities rehearsed to date
•
Ground system radio link check procedures
•
Powering on/off the CanSat
•
Launch configuration preparations (e.g., final assembly and
stowing appendages)
•
Loading the CanSat in the launch vehicle
•
Telemetry processing, archiving, and analysis
•
Recovery
•
D
e
s
c
r
i
p
t
i
o
n
o
f
w
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d
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v
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d
/
r
e
q
u
i
r
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d
CanSat 2025 CDR
: Team ### (Team Number and Name)
80
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
81
R
e
q
u
i
r
e
m
e
n
t
s
C
o
m
p
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i
a
n
c
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P
r
e
s
e
n
t
e
r
N
a
m
e
(
s
)
G
o
H
e
r
e
The purpose of this section is to summarize and cross reference the compliance to
the CanSat Competition Mission Guide requirements.
R
e
q
u
i
r
e
m
e
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t
s
C
o
m
p
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i
a
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O
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w
•
S
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•
S
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,
t
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a
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o
u
s
i
s
s
u
e
–
w
h
y
?
CanSat 2025 CDR
: Team ### (Team Number and Name)
82
Presenter: Name goes here
R
e
q
u
i
r
e
m
e
n
t
s
C
o
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p
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a
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(
m
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,
a
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)
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P
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b
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r
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q
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m
e
n
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s
–
Use the following format in as many slides as required
CanSat 2025 CDR
: Team ### (Team Number and Name)
83
Use the Green (Comply), Yellow (Partial Compliance), and Red (No Comply) color
codes as shown in the examples above for each requirement
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
84
M
a
n
a
g
e
m
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P
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(
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G
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CanSat 2025 CDR
: Team ### (Team Number and Name)
85
S
t
a
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u
s
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f
P
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c
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m
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•
P
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p
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s
–
What has been ordered, when it arrives, etc.
–
This should include flight and GCS hardware (and
software if being ordered)
•
T
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Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
86
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Cost of
each
components and hardware
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Indication of whether these costs are actual, estimates,
or budgeted values
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Indication of hardware re-use from previous years
•
The current market value for re-used components should be
included
•
Current market value of any free components, materials and
services
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Total expenses and compare to requirement(s)
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
87
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To provide an understanding of the overall design and development costs
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Get the teams thinking about the overall costs including necessary funds for travel
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Identify shortfalls in the budget that require attention
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In the past some teams have not been able to attend the competition due to a lack of funds
•
If caught early enough, there are a number of resources for funding that may available to
teams
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Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
88
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Failure to do so will result in a loss of points
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
89
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Provide tool for judges to assess trouble areas and offer ways for the team to best
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CDR: Team ### (Team Number and Name)
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CanSat 2025 CDR
: Team ### (Team Number and Name)
91
Presenter: Name goes here
CanSat 2025 CDR
: Team ### (Team Number and Name)
92
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: Team ### (Team Number and Name)
93
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: Team ### (Team Number and Name)
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CanSat 2025 CDR
: Team ### (Team Number and Name)
95
This outline provides a structured plan for the CanSat 2025 Critical Design Review (CDR) presentation, including sections on team organization, mission summary, system overview, and more. The presentation format, guidelines, and presenter information are also detailed. The content emphasizes the importance of clarity and conciseness in delivering key information to reviewers.
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Presentation Transcript
Team Logo Here CanSat 2025 Critical Design Review (CDR) Outline Version 1.0 Your Team Number Here Your Team Name Here CanSat 2025 CDR: Team ### (Team Number and Name) 1
Team Logo Here (If You Want) Presentation Outline Provide a simple outline of the presentation Indicate the team member(s) who will be presenting each section Terms: Payload refers to the Cansat IMPORTANT PRESENTATION GUIDELINE: Teams should only present slides with this star icon. Other slides should be skipped to save time; they will be reviewed by the judges off line. However, be sure to have all slides in the version presented. Presentations are to be 30 minutes in length. Going over 30 minutes will result in points lost. 2 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Team Organization Single slide listing the team members and their roles If possible, please include year (freshman, sophomore, etc.) for reference This only needs to be provided once for team members showing up multiple times on the org chart Good format is the use of an organization chart, such as below: Sample 3 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Acronyms Provide a list of acronyms used throughout the presentation During presentations, do not read through these acronyms These are for reference only 4 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here The purpose of this section is to introduce the reviewer to the overall requirements and configuration of the CanSat. This provides a basis for the details presented in the subsystem sections. System Overview Presenter Name(s) Go Here CanSat 2025 CDR: Team ### (Team Number and Name) 5
Team Logo Here (If You Want) Mission Summary Overview of the mission objectives Indicate whether selectable objective (bonus) is being attempted Describe selection rationale Include any external objectives (personal, laboratory or sponsor, class, etc.) relevant to the design 6 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Summary of Changes Since PDR Overview design changes since PDR Details of the changes are discussed in subsequent sections In every section, the summary of changes since PDR should be detailed in a separate slide, or indicate that there were no changes. 7 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) System Requirement Summary Overview of system (mission) level requirements Use bullets or a table to demonstrate an understanding of the mission requirements Do not include all requirements, just high level system level requirements the describe the overall mission The purpose of the table is to demonstrate the team understands the system-level requirements This table may be expanded to multiple tables as needed 8 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) System Concept of Operations (CONOPS) Slide(s) providing overview of CanSat operations Include: Pre-launch activities Launch and descent operations Be sure to include Payload operations Post-launch recovery and data reduction Focus on launch day activities Team member roles and responsibilities on launch day Simple flow diagrams and cartoons are a good way to present the CONOPS Absolutely no hand-drawn diagrams Photos are acceptable 9 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) CanSat Physical Layout The goal is to present the physical idea of what the CanSat will look like for reference prior to getting into details of the CanSat design Diagram(s) showing physical layout of selected CanSat configuration Make sure to include: Dimensions Placement of major components Sensors, electronics, radio, power, mechanisms Relevant configurations Payload, launch configuration, deployed, etc. 10 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Launch Vehicle Compatibility Include a dimensioned drawing that shows clearances with the payload section Focus on launch configuration Include all descent control apparatus (no sharp protrusions) What is the clearance? (Leave margin to allow easy deployment!) Notes: In past years there were a large number of CanSats that did not deploy from the payload sections of the rocket because of protrusions or because the CanSat was too wide to fit in the rocket Lack of sharp protrusions and fit within the Launch Vehicle will also be scored at the Flight Readiness Review 11 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here Sensor Subsystem Design Presenter Name(s) Go Here CanSat 2025 CDR: Team ### (Team Number and Name) 12
Team Logo Here (If You Want) Sensor Subsystem Overview One slide providing an overview of the CanSat sensor subsystem Include summary of the selected sensors (type & models) Include brief discussion of what the sensors are used for 13 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Sensor Changes Since PDR One slide providing an overview of the CanSat sensor system changes since PDR Include rationale Clearly explain why changes were made, including things like: Power limitations Testing Component size Availability 14 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Air Pressure Sensor Summary Summary of altitude sensor selection and characteristics Include: Sensor accuracy and data format Overview of data processing (including equations, as appropriate) If there is no sensor, have a page that states it to receive the points 15 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Air Temperature Sensor Summary Summary of temperature sensor selection and characteristics Include: Sensor accuracy and data format Overview of data processing (including equations, as appropriate) If there is no sensor, have a page that states it to receive the points 16 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Voltage Sensor Summary Summary of battery voltage sensor selection and characteristics Include: Sensor accuracy and data format Overview of data processing (including equations, as appropriate) 17 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload GNSS Sensor Summary Summary of GPS sensor selection and characteristics Include: Sensor accuracy and data format Overview of data formats (including equations, as appropriate) 18 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Auto-gyro Rotation Rate Sensor Summary Summary of sensors selected to determine auto-gyro blade rotation rate relative to payload structure during ascent and descent Include: Sensor accuracy and data format Overview of data formats (including equations, as appropriate) 19 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Tilt Sensor Summary Summary of sensors selected to determine payload tilt during descent Include: Sensor accuracy and data format Overview of data formats (including equations, as appropriate) 20 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Ground Camera Sensor Summary Summary of camera selection and characteristics Include: Ensure your camera meets the requirement of 640x480 pixels in color 21 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Parachute Release Camera Summary Summary of camera selection and characteristics Include: Ensure your camera meets the requirement of 640x480 pixels in color 22 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here Descent Control Design Presenter Name(s) Go Here CanSat 2025 CDR: Team ### (Team Number and Name) 23
Team Logo Here (If You Want) Descent Control Overview One slide providing an overview of the Cansat descent control system Include overview of the selected configurations and components necessary Include diagrams outlining descent control strategy for various flight altitude ranges 24 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Descent Control Changes Since PDR List changes since the PDR Include rationale Prototype testing 25 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Container Parachute Descent Control Summary Describe payload descent control hardware Include details on parachute design Shape selection Size selection color etc This discussion can carry over to multiple slides if necessary 26 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Auto-gyro Descent Control Summary Describe how design of auto-gyro in relation to descent control. shape size expected rotation rate aerodynamics 27 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Auto-gyro Descent Stability Control Design Describe how the payload is kept stable and not tumble Describe mechanisms used Describe how payload is kept nadir pointing Show design of method Active or passive stability control 28 28 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Descent Rate Estimates Present descent rate estimates for the following CanSat configurations Parachute Auto-gyro Include discussion of Calculations used Assumptions This discussion can carry over to multiple slides if necessary Last slide summarizes results. Make sure final results are clearly identified. 29 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here Mechanical Subsystem Design Presenter Name(s) Go Here CanSat 2025 CDR: Team ### (Team Number and Name) 30
Team Logo Here (If You Want) Mechanical Subsystem Overview One slide providing overview of the mechanical subsystem Include overview of major structural elements, material selection, and interface definitions 31 31 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Mechanical Subsystem Changes Since PDR Highlight mechanical changes since PDR. Details should be discussed on subsequent slides 32 32 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name) CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Cansat Mechanical Layout of Components Show structure (CAD model) include dimension drawings Identify location of electrical components Identify major mechanical parts mechanisms such as springs, hinges, etc. Structural material selection(s) 33 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Container Design Show and explain container design. Show any changes from reference design Show dimensions including required dimensions How is shoulder dimensions verified for proper fit 34 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Pre-Deployment Configuration Show payload in pre-deployed configuration Explain how payload is secured in container. 35 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Release Show and explain how payload is released from container. Mechanisms used for release Sequence of operation for release Trigger for release 36 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Deployment Configuration Show and explain any mechanisms and/or structures that change or open when payload is released. Not the auto-gyro. If none, state no change in payload structure 37 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Auto-gyro deployment Show and explain how auto-gyro mechanism is deployed. Show mechanisms Sequence of deployment 38 Presenter: Name goes here CanSat 2025 PDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Ground Camera Pointing Show and explain how camera points north during descent Show mechanisms Explain operations Pointing algorithms if any 39
Team Logo Here (If You Want) Structure Survivability As applicable for the Cansat, discuss: Electronic component mounting methods Electronic component enclosures Acceleration and shock force requirements and testing Securing electrical connections (glue, tape, etc.) Consider required judge verification during pre-flight check in Descent control attachments 40 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Mass Budget Table(s) providing the following: Mass of each component of the Cansat Mass of each structural element Sources/uncertainties whether the masses are estimates, from data sheets, measured values, etc. Total mass of all components and structural elements Margin : The amount of mass (in grams) in which the mass budget meets, exceeds, or falls short of the mass requirement Method of correction to meet mass requirement (based on the margin listed above) 41 Presenter: Name goes herec CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here Communication and Data Handling (CDH) Subsystem Design Presenter Name(s) Go Here CanSat 2025 CDR: Team ### (Team Number and Name) 42
Team Logo Here (If You Want) CDH Overview One slide providing overview of the CDH subsystem Should include selected components (with brief mention of what each component is for) 43 43 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name) CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) CDH Changes Since PDR List changes to the CDH since PDR. Details of the changes should be discussed in subsequent slides 44 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Processor & Memory Selection Include boot time Include processor speed Include data interfaces (types and numbers) Include memory storage requirements, if applicable 45 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Real-Time Clock Describe design for Payload real-time clock Hardware clock with independent power supply Reset tolerance Real time clock should have independent battery backup to maintain time through power transients 46 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Antenna Selection Description and characteristics of the antenna selected for the CanSat Discuss: Performance Mass 47 47 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name) CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Radio Configuration XBEE radio selection NETID setting Include transmission control How is this managed during each mission phase? Note: Communications failures have occurred often over the past several years of the competition You are encouraged to use your radios in all of your development and testing to better ensure mission success Ideally you have started working with the radio and communications protocol Start Radio Prototyping and Testing Early! 48 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Telemetry Format What data is included? Check the competition guide for telemetry requirements Data rate of packets? How is data formatted? Include example frames with complete descriptions Does the presented format match the Competition Guide requirements? 49 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
Team Logo Here (If You Want) Payload Command Formats List all supported commands with examples What data is included? Check the competition guide for command requirements How is command data formatted? Include example commands with complete descriptions Does the presented format match the Competition Guide requirements? 50 Presenter: Name goes here CanSat 2025 CDR: Team ### (Team Number and Name)
