| Literature DB >> 24923426 |
Junya Ikuta1, Nagendra K Kamisetty1, Hirofumi Shintaku1, Hidetoshi Kotera1, Takahide Kon2, Ryuji Yokokawa3.
Abstract
Intracellular cargo is transported by multiple motor proteins. Because of the force balance of motors with mixed polarities, cargo moves bidirectionally to achieve biological functions. Here, we propose a microtubule gliding assay for a tug-of-war study of kinesin and dynein. A boundary of the two motor groups is created by photolithographically patterning gold to selectively attach kinesin to the glass and dynein to the gold surface using a self-assembled monolayer. The relationship between the ratio of two antagonistic motor numbers and the velocity is derived from a force-velocity relationship for each motor to calculate the detachment force and motor backward velocity. Although the tug-of-war involves >100 motors, values are calculated for a single molecule and reflect the collective dynein and non-collective kinesin functions when they work as a team. This assay would be useful for detailed in vitro analysis of intracellular motility, e.g., mitosis, where a large number of motors with mixed polarities are involved.Entities:
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Year: 2014 PMID: 24923426 PMCID: PMC4055898 DOI: 10.1038/srep05281
Source DB: PubMed Journal: Sci Rep ISSN: 2045-2322 Impact factor: 4.379
Figure 1Selective kinesin and dynein patterning.
(a) Schematic for selective coating procedure of kinesin and dynein. (1) Biotinylated SAM grafting on the gold patterned region. (2) Kinesin, (3) streptavidin, and (4) dynein were immobilized sequentially. Selective coating was examined by injecting (5) PMMT, and the gliding direction was evaluated (6). (b), (c) PMMTs gliding on the selectively immobilized motors in the (b) SAM-coated region (led by dimmer plus end) and (c) glass region (led by brighter minus end). Scale bar, 10 μm. (d), (e) Polarity of PMMTs gliding on the (d) SAM-coated region and (e) glass region. Control surfaces were prepared by omitting kinesin in (d) or dynein in (e) from the optimum assay for the selective coating. In both cases, polarity distribution was not significantly different (p > 0.05) from control experiments as determined with the chi-square test. n.s. = not significant.
Figure 2Behavior of MTs at the dynein-kinesin boundary.
(a) Schematic diagram for grouping MT behavior. MTs approached the boundary from the dynein-coated region (group 1) or the kinesin-coated region (group 2). The tip of the MT was at the boundary with the minus end in the dynein-coated region (group 3) or in the kinesin-coated region (group 4). θ is the approach angle of the tip of the MT to the boundary. (b), (c) The behavior of MTs with respect to the approach angle, θ. MTs approached from (b) the dynein-coated region and (c) the kinesin-coated region. Values are the mean ± s.d. (n = 286 for (b) and n = 168 for c).
Figure 3Tug-of-war of MTs at the boundary of a kinesin- and dynein-patterned surface.
(a), (b) MTs experiencing tug-of-war and glide to the (a) kinesin-coated region and (b) dynein-coated region. Scale bar, 10 μm. (c), (d) Normalized MT length and velocity during tug-of-war for MTs gliding to (c) the kinesin-coated region (n = 7) and (d) the dynein-coated region (n = 4). Ratio of the MT length attached to the “winning” motor region (blue plots) and normalized velocity (red plots). The standard velocity for each MT that was measured when the MT passed the boundary and was propelled only by the “winning” motors at t = 0 was used to calculate the normalized velocity. Dimensionless time is defined as (elapsed time)/(MT length)/(standard MT velocity). The same symbols are used for a MT in each graph. (e), (f) Relationship between velocity and ratio of the motor number. (e) N/N–velocity and (f) N/N–velocity relationships for MTs gliding to the kinesin- and dynein-coated regions, respectively. Velocity was normalized as described above. MTs that were analyzed here correspond to those that were tracked in Fig. 3c,d and are coded accordingly. Fitted curves based on the three models are shown.
Parameters obtained by fitting the F-V relationships to experimental results
| Model type | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Model 1 (Proportional load model) | 0.94 | 1.4 | 6 | 1.1 | 1.5 | 5.6 | 0.24 | 0.41 | NA | NA |
| Model 2 (Linear F-V model) | 0.27 | 2.2 | 6 | 1.1 | 2.4 | 1.6 | 1 | 1 | 503 | 9.5 |
| Model 3 (Non-linear F-V model) | 0.5 | 2.1 | 6 | 1.1 | 2.3 | 3.0 | 2 | 0.5 | 456 | 56 |
| Kunwar | 0.19 | 2.9 | 4.7 | 1.4 | 4.0 | 0.87 | 2 | 0.5 | NA | NA |
| Muller | 0.13 | 2.7 | 6 | 1.1 | 3 | 0.75 | 1 | 1 | 6 | 72 |
f, dynein stall force, f, kinesin stall force, f, dynein detachment force, f, kinesin detachment force, w, linear/nonlinear parameter for kinesin, w, linear/nonlinear parameter for dynein, v, kinesin backward velocity, v, dynein backward velocity, NA, not applicable.