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1. Tilt-to-length coupling in LISA Pathfinder: A data analysis

2. Charging of free-falling test masses in orbit due to cosmic rays: Results from LISA Pathfinder

3. Sensor noise in LISA Pathfinder : An extensive in-flight review of the angular and longitudinal interferometric measurement system

4. Temperature stability in the sub-milliHertz band with LISA Pathfinder

5. Sensor Noise in LISA Pathfinder : In-Flight Performance of the Optical Test Mass Readout

6. Analysis of the Accuracy of Actuation Electronics in the Laser Interferometer Space Antenna Pathfinder

7. Novel methods to measure the gravitational constant in space

8. LISA Pathfinder Performance Confirmed in an Open-Loop Configuration: Results from the Free-Fall Actuation Mode

9. LISA Pathfinder micronewton cold gas thrusters: In-flight characterization

10. LISA Pathfinder platform stability and drag-free performance

11. Forbush Decreases and

12. Experimental results from the ST7 mission on LISA Pathfinder

13. Precision charge control for isolated free-falling test masses: LISA pathfinder results

14. Calibrating the system dynamics of LISA Pathfinder

15. Beyond the Required LISA Free-Fall Performance: New LISA Pathfinder Results down to 20 μHz

16. In-flight testing of the injection of the LISA Pathfinder test mass into a geodesic

17. Capacitive sensing of test mass motion with nanometer precision over millimeter-wide sensing gaps for space-borne gravitational reference sensors

18. Charge-Induced Force Noise on Free-Falling Test Masses: Results from LISA Pathfinder

19. Sub-Femto-gFree Fall for Space-Based Gravitational Wave Observatories: LISA Pathfinder Results

20. Analysis of the accuracy of actuation electronics in the laser interferometer space antenna pathfinder

21. Spacecraft and interplanetary contributions to the magnetic environment on-board LISA Pathfinder

22. LISA Pathfinder platform stability and drag-free performance

23. Forbush decreases and <2 day GCR flux non-recurrent variations studied with LISA pathfinder

24. LISA Pathfinder Performance Confirmed in an Open-Loop Configuration: Results from the Free-Fall Actuation Mode

25. Novel methods to measure the gravitational constant in space

26. Micrometeoroid Events in LISA Pathfinder

27. LISA Pathfinder micronewton cold gas thrusters: In-flight characterization

28. Temperature stability in the sub-milliHertz band with LISA Pathfinder

29. Towards Galileo + GPS seismology: Validation of high-rate GNSS-based system for seismic events characterisation

30. Precision charge control for isolated free-falling test masses: LISA pathfinder results

31. Calibrating the system dynamics of LISA Pathfinder

32. Beyond the required LISA free-fall performance: new LISA Pathfinder results down to 20 μHz

33. Characteristics and Energy Dependence of Recurrent Galactic Cosmic-Ray Flux Depressions and of a Forbush Decrease with LISA Pathfinder

34. Experimental results from the ST7 mission on LISA Pathfinder

35. Measuring the Galactic Cosmic Ray Flux with the LISA Pathfinder Radiation Monitor

36. LISA Pathfinder closed-loop analysis: a model breakdown of the in-loop observables

37. LISA Pathfinder: First steps to observing gravitational waves from space

38. Charge-induced force noise on free-falling test masses: results from LISA Pathfinder

39. Sub-Femto- g Free Fall for Space-Based Gravitational Wave Observatories: LISA Pathfinder Results

40. Detection of a Sea Surface Salinity Gradient Using Data Sets of Airborne Synthetic Aperture Radiometer HUT-2-D and a GNSS-R Instrument

41. AMIRAS—An Airborne MIRAS Demonstrator

42. The Flat Target Transformation

43. Free-flight experiments in LISA Pathfinder

44. In-flight thermal experiments for LISA Pathfinder: Simulating temperature noise at the Inertial Sensors

45. Disentangling the magnetic force noise contribution in LISA Pathfinder

46. A noise simulator for eLISA: Migrating LISA Pathfinder knowledge to the eLISA mission

47. Bayesian statistics for the calibration of the LISA Pathfinder experiment

48. SMOS calibration and instrument performance after one year in orbit

49. SMOS instrument performance and calibration

50. Smos payload performance assessment

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