Similarity Design Method of the Inflatable Buffer Landing System

Table 4

Comparison of the overloading of the prototype and the full-scale system for the Mars Pathfinder.

Case	Peak overloading (g)	Error (%)	Peak times (s)	Error (%)	Pulse width (s)	Error (%)
Full scale	30.92	—	0.2653	—	0.205	—
Prototype	33.85	9.48	0.2615	1.43	0.2031	0.92