Bistable tape springs are ultrathin fiber-reinforced polymer composites, which could self-deploy through releasing stored strain energy. Strain energy relaxation is observed after long-term stowage of bistable tape springs due to viscoelastic effects and the tape springs might lose their self-deployment abilities. In order to mitigate the viscoelastic effects and thus ensure self-deployment, different tape springs were designed, manufactured, and tested. Deployment experiments show that a four-layer, [−45/0/90/45], plain weave glass fiber tape spring has a high capability to mitigate the strain energy relaxation effects to ensure self-deployment after long-term stowage in a coiled configuration. The two inner layers increase the deployment force and the outer layers are used to generate the bistability. The presented four-layer tape spring can self-deploy after more than six months of stowage at room temperature. A numerical model was used to assess the long-term stowage effects on the deployment capability of bistable tape springs. The experiments and modeling results show that the viscoelastic strain energy relaxation starts after only a few minutes after coiling. The relaxation shear stiffness decreases as the shear strain increases and is further reduced by strain energy relaxation when a constant shear strain is applied. The numerical model and experiments could be applied in design to predict the deployment force of other types of tape springs with viscoelastic and friction effects included.

References

1.
Iqbal
,
K.
, and
Pellegrino
,
S.
,
2000
, “
Bi-Stable Composite Shells
,”
AIAA
Paper No. 2000-1385.
2.
Schultz
,
M. R.
,
Hulse
,
M. J.
,
Keller
,
P. N.
, and
Turse
,
D.
,
2008
, “
Neutrally Stable Behavior in Fiber-Reinforced Composite Tape Springs
,”
Composites, Part A
,
39
(
6
), pp.
1012
1017
.
3.
Jeon
,
S. K.
, and
Murphey
,
T. W.
,
2011
, “
Design and Analysis of a Meter-Class CubeSat Boom With a Motor-Less Deployment by Bi-Stable Tape Springs
,”
AIAA
Paper No. 2011-1731.
4.
Murphey
,
T. W.
,
Francis
,
W. H.
,
Davis
,
B. L.
,
Mejia-Ariza
,
J.
,
Santer
,
M.
,
Footdale
,
J. N.
,
Schmid
,
K.
,
Soykasap
,
O.
, and
Koorosh
,
G.
,
2015
, “
High Strain Composites
,”
AIAA
Paper No. 2015-0942.
5.
Mobrem
,
M.
, and
Adams
,
D.
,
2009
, “
Deployment Analysis of the Lenticular Jointed Antennas Onboard the Mars Express Spacecraft
,”
J. Spacecr. Rockets
,
46
(
2
), pp.
394
402
.
6.
Mobrem
,
M.
, and
Adams
,
D.
,
2009
, “
Lenticular Jointed Antenna Deployment Anomaly and Resolution Onboard the Mars Express Spacecraft
,”
J. Spacecr. Rockets
,
46
(
2
), pp.
403
410
.
7.
Domber
,
J. L.
,
Hinkle
,
J. D.
,
Peterson
,
L. D.
, and
Warren
,
P. A.
,
2002
, “
Dimensional Repeatability of an Elastically Folded Composite Hinge for Deployed Spacecraft Optics
,”
J. Spacecr. Rockets
,
39
(
5
), pp.
646
652
.
8.
Soykasap
,
Ö.
,
2009
, “
Deployment Analysis of a Self-Deployable Composite Boom
,”
Compos. Struct.
,
89
(
3
), pp.
374
381
.
9.
Brinkmeyer
,
A.
,
Pellegrino
,
S.
, and
Weaver
,
P. M.
,
2015
, “
Effects of Long-Term Stowage on the Deployment of Bistable Tape Springs
,”
ASME J. Appl. Mech.
,
83
(
1
), p.
011008
.
10.
Mallikarachchi
,
H. M. Y. C.
, and
Pellegrino
,
S.
,
2014
, “
Deployment Dynamics of Ultrathin Composite Booms With Tape-Spring Hinges
,”
J. Spacecr. Rockets
,
51
(
2
), pp.
604
613
.
11.
Kwok
,
K.
, and
Pellegrino
,
S.
,
2013
, “
Folding, Stowage, and Deployment of Viscoelastic Tape Springs
,”
AIAA J.
,
51
(
8
), pp.
1908
1918
.
12.
Kwok
,
K.
, and
Pellegrino
,
S.
,
2017
, “
Micromechanics Models for Viscoelastic Plain-Weave Composite Tape Springs
,”
AIAA J.
,
55
(
1
), pp.
309
321
.
13.
Mallol
,
P.
,
2013
, “
Deployment Simulations of a Composite Boom for Small Satellites
,”
Licentiate thesis
, KTH Royal Institute of Technology, Stockholm, Sweden.
14.
Guest
,
S.
, and
Pellegrino
,
S.
,
2006
, “
Analytical Models for Bistable Cylindrical Shells
,”
Proc. R. Soc. A
,
462
(
2067
), pp.
839
854
.
15.
Hyer
,
M. W.
,
1981
, “
Some Observations on the Cured Shape of Thin Unsymmetric Laminates
,”
J. Compos. Mater.
,
15
(
2
), pp.
175
194
.
16.
Peterson
,
M. E.
, and
Murphey
,
T. W.
,
2013
, “
Large Deformation Bending of Thin Composite Tape Spring Laminates
,”
AIAA
Paper No. 2013-1667.
17.
Murphey
,
T. W.
,
Peterson
,
M. E.
, and
Grigoriev
,
M. M.
,
2013
, “
Four Point Bending of Thin Unidirectional Composite Laminas
,”
AIAA
Paper No. 2013-1668.
18.
Hexcel
,
2014
, “
Hexply M77 Product Data Sheet
,” Hexcel Corporation, Stamford, CT, accessed May 19, 2017, http://www.hexcel.com/user_area/content_media/raw/HexPly_M77_eu_DataSheet.pdf
20.
Mao
,
H.
,
Ganga
,
P. L.
,
Ghiozzi
,
M.
,
Ivchenko
,
N.
, and
Tibert
,
G.
,
2017
, “
Deployment of Bistable Self-Deployable Tape Spring Booms Using a Gravity Offloading System
,”
J. Aerosp. Eng.
,
30
(4), p.
04017007
.
21.
ASTM International
,
2014
, “
Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials
,” ASTM International, West Conshohocken, PA, Standard No.
ASTM D3039/D3039M-14
.
22.
ASTM International
,
2013
, “
Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45° Laminate
,” ASTM International, West Conshohocken, PA, Standard No.
ASTM D3518/D3518M-13
.
23.
Tuttle
,
M. E.
, and
Brinson
,
H. F.
,
1986
, “
Prediction of the Long-Term Creep Compliance of General Composite Laminates
,”
Exp. Mech.
,
26
(
1
), pp.
89
102
.
24.
Rimrott
,
F.
,
1967
, “
Stem Self-Extension Velocities
,”
Can. Aeronaut. Space J.
,
13
(
1
), pp.
1
7
.
You do not currently have access to this content.