Department of Biomedical Engineering, Texas A&M University, College Station, TX 77843, USA.
Bone. 2013 Jan;52(1):433-43. doi: 10.1016/j.bone.2012.09.021. Epub 2012 Sep 24.
Profound bone loss at weight bearing sites is a primary effect of long-duration spaceflight. Moreover, a significant increase in estimated fracture risk remains even 1 year after returning to Earth; hence, it is important to define how quickly bone integrity can recover following prolonged disuse. This study characterized the loss and recovery dynamics of bone following a period of rodent hindlimb unloading in three anatomic sites. We hypothesized that the rat femoral neck would exhibit a discordant recovery dynamic most similar to that observed in astronauts' proximal femur; that is, bone mineral content (absolute mass) at this site would recover faster and more completely than would bone density and cortical area, and they will all recover before bone strength does. We characterized loss and long-term recovery of densitometric properties at the femoral neck, proximal tibia metaphysis, and tibia diaphysis, and also mechanical properties at the femoral neck and tibia diaphysis for which mechanical testing is amenable. We assessed the relationship between calculated strength indices and measured mechanical properties. Adult male Sprague-Dawley rats (6 months) were assigned to baseline, age-matched control (AC), and hindlimb unloaded (HU) groups. The HU group was unloaded for 28 days and then returned to normal cage activity for 84 days of weight bearing recovery (3 times the duration of HU). Fifteen animals were euthanized from each of the HU and AC groups on days 28, 56, 84, and 112 of the study. At baseline and then every 28 days in vivo longitudinal pQCT scans were taken at proximal tibia metaphysis (PTM) and tibia diaphysis (TD); ex vivo pQCT scans were taken later at the femoral neck (FN). TD and FN were tested to failure to measure mechanical properties. The hypothesis that the femoral neck in rats will exhibit a discordant recovery dynamic most similar to that observed in astronauts' proximal femurs was not supported by our data. At the femoral neck, densitometric and geometric variables (total BMC, total vBMD, cancellous vBMD, and cortical area) recovered to age-matched control levels after a recovery period twice the duration of unloading. Contrary to our hypothesis, changes in densitometric variables at the PTM provided a better model for changes in the human femoral neck with prolonged weightlessness. Following 28 days of HU, PTM total BMC recovered to age-matched control levels after roughly two times the duration of unloading; however, total vBMD did not recover even after three recovery periods. Cortical thinning occurred at the PTM following HU likely due to inhibition of periosteal growth; cortical shell thickness did not recover even after three recovery periods. Calculated strength indices suggested a loss in strength at the tibial diaphysis, which was not confirmed with direct testing of mechanical properties. HU had no effect on maximum fracture force at mid-tibia diaphysis; however, femoral neck experienced a significant loss of maximum force due to unloading that fully recovered after 28 days. Estimated strength indices for the femoral neck suggested a recovery period of 56 days in contrast to the 28-day recovery that was observed with mechanical testing. However, the inaccuracy of strength indices vs. directly measured mechanical properties highlights the continued importance of ground based animal models and mechanical testing. Our results demonstrate that the PTM in the rat better matches loss and recovery dynamics observed in astronauts' proximal femur than does the rat FN, at least in terms of densitometric variables. More complete utility of the rat PTM as a model in this case, however, depends upon meaningful characterization of changes in mechanical properties as well.
承重部位的严重骨质流失是长期太空飞行的主要影响。此外,即使在返回地球一年后,估计的骨折风险仍显著增加;因此,确定在长期不活动后骨骼完整性恢复的速度非常重要。本研究在三个解剖部位描述了啮齿动物后肢去负荷后骨的丢失和恢复动态。我们假设大鼠股骨颈将表现出与宇航员股骨近端最相似的不一致恢复动态;也就是说,该部位的骨矿物质含量(绝对质量)的恢复速度更快,更完全,而骨密度和皮质面积的恢复速度较慢,而且所有这些都将在骨强度恢复之前恢复。我们描述了股骨颈、胫骨近端干骺端和胫骨骨干的密度特性以及股骨颈和胫骨骨干的机械性能的丢失和长期恢复情况,对于可进行机械测试的部位则可以进行机械性能测试。我们评估了计算出的强度指数与测量的机械性能之间的关系。成年雄性 Sprague-Dawley 大鼠(6 个月)分为基线、年龄匹配的对照组(AC)和后肢去负荷组(HU)。HU 组去负荷 28 天,然后恢复正常笼内活动 84 天进行承重恢复(HU 时间的 3 倍)。研究的第 28、56、84 和 112 天,每组从 HU 和 AC 组中处死 15 只动物。在基线以及随后的 28 天内,对胫骨近端干骺端(PTM)和胫骨骨干(TD)进行了体内纵向 pQCT 扫描;后来对股骨颈(FN)进行了体外 pQCT 扫描。TD 和 FN 进行了破坏试验以测量机械性能。大鼠股骨颈将表现出与宇航员股骨近端最相似的不一致恢复动态的假设并未得到我们数据的支持。在股骨颈,骨密度和几何变量(总 BMC、总 vBMD、松质 vBMD 和皮质面积)在恢复期间恢复到与年龄匹配的对照组水平,恢复时间是去负荷时间的两倍。与我们的假设相反,在长时间失重的情况下,PTM 的骨密度变化为人类股骨颈的变化提供了更好的模型。在 HU 后 28 天,PTM 总 BMC 在去负荷后大约两倍的时间内恢复到与年龄匹配的对照组水平;然而,总 vBMD 甚至在三个恢复周期后都没有恢复。HU 后 PTM 发生皮质变薄,可能是由于骨膜生长受到抑制;皮质壳厚度甚至在三个恢复周期后都没有恢复。计算出的强度指数表明胫骨骨干的强度降低,但直接进行机械性能测试并未证实这一点。HU 对中胫骨骨干的最大断裂力没有影响;然而,由于去负荷,股骨颈的最大力显著下降,28 天后完全恢复。股骨颈的估计强度指数表明恢复时间为 56 天,而机械测试观察到的恢复时间为 28 天。然而,强度指数与直接测量的机械性能之间的不准确性突出表明,地面动物模型和机械测试仍然非常重要。我们的结果表明,与大鼠 FN 相比,大鼠 PTM 至少在骨密度变量方面更好地匹配了宇航员股骨近端观察到的丢失和恢复动态。然而,要使大鼠 PTM 更充分地作为模型使用,还取决于对机械性能变化的有意义的描述。