Transcript Powerpoint

Dynamics & Control - Tether
Critical Design Review
Anne DeLion
27 February 2001
Tether Type - Multiline
 Multi-line Tether
 Weight is comparable
to a single line tether
 High redundancy
Survival probability of a failsafe multiline tether
versus an equal-mass single line tether
 The number of lines is
proportional to
redundancy
 Very high survivability
 Hoytether structure is
less likely to tangle on
deployment
Hoyt, R. and Forward, R. “The HoytetherTM:
A Failsafe Multiline Space Tether Structure.”
www.tethers.com
Tether Specifications
Material: Spectra 2000
Safety Factor: 5 (minimum)
HAB
ERV
Length (m)
324.38
1003.5
Maximum Tension (N)
279600
342400
Diameter (m)
0.0225
0.0249
Mass (kg)
125.32
474.73
Stretch (m)
1.339
4.144
Deployment Reel Mass (kg)
~ 130
~ 500
Reel Dimensions (m)
.5r x 3l
.5r x 3l
Total Tether/Reel Volume (m^3)
2.49
2.85
Total Tether/Reel Mass (kg)
~255
~975
Hab Tether/Cable Specifications
Tether Material: Spectra 2000
Cable: 2210 kg/km
Safety Factor: 5 (minimum)
HAB
Length (m)
356.8
Maximum Tension (N)
279600
Diameter (m)
0.1
Mass (kg)
2491
Deployment Reel Mass (kg)
~ 2500
Reel Dimensions (m)
.5r x 3l
Total Tether/Reel Volume (m^3)
5.15
Total Tether/Reel Mass (kg)
~5000
ERV Tether
ERV Tether Mass versus g Force Loads
[Anne DeLion]
600
Vary Angular Velocity; ERV Distance to CM is constant = 223 m
Vary ERV Distance to CM; Angular Velocity is constant = 2rpm
Tether Mass (kg)
500
400
300
200
100
0
0.4
0.5
0.6
0.7
0.8
g Force
0.9
1
1.1
Hab Deployment & Spin-up
 Three-Step Deployment Method
1. Thrust to spin up the connected vehicle system to the
desired initial spin rate
2. Stop thrust, release vehicles, and conservation of
angular momentum will deploy the tether
3. After tether is completely deployed, thrust to spin the
system up to 2 rpm for artificial gravity
Note: Thrusting is done on both the Hab and NTR. The
thrust is proportional so moments about cm cancel.
Also, by doing some thrusting on the NTR less
propellent is used.
Hab Deployment & Spin-up Numbers
Hab Thrust = ~660 N
NTR Thrust = ~250 N
Initial Spin-up
Artificial Gravity Spin-up
Burn Time (hh:mm:ss)
00:22:26
08:20:53
Max G Force Generated
1.22g
.38g
Max Vtangential (m/s)
29.4
17.8
• If the tether is cut during the 2rpm spin:
Imparted DV = 17.8 m/s
Hab Tether Deployment
 Tether Deployment
 Thrust = 0 N
 Tension is kept on tether by centripetal force
 Deployment time = 1 hour
 Is arbitrary and can be set longer/shorter
 Mechanism to control deployment rate is black-boxed
in reel system
 Final spin rate after deployment = 0.017 rpm
ERV Deployment & Spin-up
 Three-Step Deployment Method
 Use same method as the Hab
 One significant difference:
ERV will initially spin up to .38g. At some
point in the mission, the ERV will spin up
.02g additional each day for 31 days to
finally create 1g
ERV Deployment & Spin-up Numbers
ERV Thrust = ~660 N
MLV Thrust = ~250 N
Initial Spin-up
.38g Spin-up
.02g Spin-up
Total g Spin-up
Burn Time
(hh:mm:ss)
00:20:17
01:17:49
00:17:51
10:31:13
Max G Force
Generated
1g
.38g
.02g additional
1g
Max Vtangential
(m/s)
14.0
28.8
-
46.7
• If the tether is cut during .38g phase of spin:
Imparted DV = 28.8 m/s
• If the tether is cut during 1g phase of spin:
Imparted DV = 46.7 m/s
ERV 1g Spin-up
Total Angular Velocity of ERV System versus g Force Loads
[Anne DeLion]
0.21
0.2
Angular Velocity (rad/s)
0.19
0.18
0.17
0.16
0.15
0.14
0.13
0.12
0.3
0.4
0.5
0.6
0.7
g Force
0.8
0.9
1
1.1
ERV 1g Spin-up
G Force Loads Over the ERV Spin-up Duration
[Anne DeLion]
1
0.9
G Force
0.8
0.7
0.6
0.5
0.4
0.3
0
5
10
15
20
Days
25
30
35
Tether Cost/Risk
 Manufacturing Cost: $1000/kg
 Hab Tether: $255 000
 ERV Tether: $975 000
 Success Probability
 Hoytether > 95%
 Avoiding catches in tether winding > 95%
 Due to greater than 10 N pulling out tether.[Hoyt]
ERV 1g Spin-up
Total Angular Velocity of ERV System versus Burn Time for Each .02g Burn
[Anne DeLion]
0.22
0.21
Angular Velocity (rad/s)
0.2
0.19
0.18
0.17
0.16
0.15
0.14
0.13
75
80
85
90
95
100
105
Burn Time (s)
110
115
120
125
ERV 1g Spin-up
Time of Each .02g Incremental Burn versus Total g Force Load
[Anne DeLion]
125
120
115
Time (s)
110
105
100
95
90
85
80
75
0.3
0.4
0.5
0.6
0.7
g Force
0.8
0.9
1
1.1
Tether Cost/Risk
 Manufacturing Cost: $1000/kg
 Hab Tether: $255 000
 ERV Tether: $975 000
 Success Probability
 Hoytether > 95%
 Avoiding catches in tether winding > 95%
 Due to greater than 10 N pulling out tether.[Hoyt]
 Mechanical Risk = ??