Mirror Transport Mechanism at Cryogenic Temperatures
Eight-flex-pivot four-bar linkage for the FIRAS experiment on COBE
Kenneth W. Stark & Meredith Wilson
Overview
The Mirror Transport Mechanism (MTM) supports a pair of dihedral mirrors and moves them in a very smooth, uniform scanning motion normal to a beamsplitter, with a quick flyback and repeat. Designed as a basic four-bar linkage connected by eight flexural pivots, the MTM operates at 1.8 K inside the FIRAS instrument on the COBE spacecraft, with a strict 5 mW power budget to minimize cryogen boil-off.
Key Highlights
1.8 K Operation
Operates inside a superfluid helium dewar for over a year in orbit
Eight Flex Pivots
Four-bar linkage upgraded from six to eight pivots for platform rigidity
INCO 718 Flex Pivots
Selected for cryogenic impact resistance (~27 N·m)
5 mW Power Budget
Lifetime reduced ~3 days per mW of dissipation
20M+ Cycle Life Test
Flex pivots life-tested for 20+ million cycles at LHe temperature
Passive Linear Motor
Only moving part is completely passive — no contact, no flexing wires
Performance Requirements
- Slow scan: 0.228 cm/sec
- Rapid scan: 0.342 cm/sec
- Flyback: ≥1.5 cm/sec
- Power dissipation: <5 mW
- Operating temperature: 1.8 K
- 26-g load vector design criteria
- Jitter: 40 µsec
- Long scan travel: 0.096 to 1.638 cm
- Short scan travel: 0.4096 to 0.102 cm
Selection Process
Three mechanisms were evaluated: a linear ball slide, a flexural-pivot four-bar linkage, and a magnetic suspension platform. The linear ball slide (stainless steel rods, then hard-coated aluminum with Teflon) had unacceptably high noise on each sweep. The magnetically suspended platform was smooth and frictionless but complex. The flex-pivot four-bar linkage was chosen for its very smooth operation, extremely low power dissipation, and simplicity of design.
Mechanical Design
The MTM was upgraded from a six-flex-pivot to an eight-flex-pivot four-bar linkage to increase rigidity of the dihedral mirror platform support. Each link has line-bored holes for true coaxial pivot centerlines, eliminating rotational stresses from misalignment. Flex pivots are captivated by slotted, clamped holes — at LHe temperature, aluminum's ΔL/L (0.0043) exceeds stainless steel's (0.003), so clamping force increases on cooldown. INCO 718 was selected for the flex pivots for its cryogenic impact resistance (~20 ft-lb).
Latch & Drive Systems
A latch mechanism captivates all moving components during launch and uncages in orbit. A 15° stepper motor through a 24:1 gear ratio drives V-shaped bearings against beryllium copper leaf springs, producing ~311 N (70 lb) of force reacted by hard-anodized cone-and-socket latches. The motor has dual windings for redundancy. The scan is driven by a unique linear motor whose only moving part is completely passive. An optical encoder (50 lines/mm grating pair) generates pulses every 20 µm to control scan reversal and trigger A/D sampling.
Mirror Transport Mechanism at Cryogenic Temperatures — PDF
Download the full paper or document for offline reference.
Have questions about this application or need engineering support?