Linear pyrolysis experimental data have been used as surface boundary conditions in the analytical treatment of solid propellant combustion problems. The surface boundary conditions required for the analysis are functional relationships between normal regression velocity, gaseous reactant density, total pressure, temperature, and possibly derivatives of these quantities as well, evaluated at the interface between condensed and gaseous phases during combustion. Available experimental data indicates that a relation based upon equilibrium conditions prevailing at the interface is not generally valid. There are available for many substances, however, hot-plate linear pyrolysis data which give an explicit relation between regression velocity of the condensed phase and a measured hot-plate temperature. This hot-plate temperature has been assumed to be also the temperature at the interface. However, this assumption is thought in some cases to be questionable. In addition, the use of such a rate law in combustion analysis would imply that the total pressure and the gascous reactant partial pressures or densities, which are greatly different for the pyrolysis test as compared to the combustion, have a negligible effect on the rate. This implication again is questionable. The present paper seeks to answer in part these questions on the validity of using linear pyrolysis data. A one-dimensional hot-plate linear pyrolysis experiment is proposed which uses a porous heated plate in place of the present impervious plate. The proposed experiment, having simpler fluid dynamics than present hot-plate experiments, is capable of a reasonably precise analytical description. The analysis is carried out for a general case and is then specialized to simple and chainlike surface gasification processes. Conditions are developed to determine whether the surface process is either a rate process or is one of near-equilibrium. A description is presented of the possible use of data from the proposed pyrolysis experiments to compute the accommodation coefficient and the vacuum sublimation rate as functions of surface temperature. With this information, the surface boundary condition for a given material will then be specified. The pyrolysis rate of potassium chloride is calculated as an example of the use of the derived formulas. If fluid dynamic effects are not too important in the present experiments, and in some respects it is estimated that they are not, interpretation from the results of this analysis serves present pyrolysis data as well. Interpretations are carried out for a number of compounds which have interest in propellant combustion studies. From published data on ammonium perchlorate, for example, revised values are estimated for the heat of sublimation, for the activation energy in linear pyrolysis, and for the difference between the hot-plate temperature and the surface temperature in linear pyrolysis.