The basic applications of pulsed solid state power amplifler are for airborne and spaceborne pulsed Radar and these applications have always demanded well performance over difierent environmental conditions. The success of the electronic systems for these applications relies on the ability to design high performance; reliable and high yield circuits, which will function against the demanded environmental speciflcations. This paper describes the detailed design and development of a spaceborne C-band pulsed solid state power amplifler to deliver 12-watt output power, 45dB gain with 22 microsecond pulse width and 8% duty cycle. The salient features of this paper are drain modulated pulse driver circuit design, non- linear design of the power stages and electronic package design. The paper also describes pulsed SSPA conflguration, RF section, Electronic Power Converter Module, RF design and other space aspects to realize the pulsed solid state power amplifler. It is fabricated on the three- layer metallized alumina substrate, integrated with power converter module; and tested under simulated space environment. The test result validates the design speciflcation of the pulsed solid state power amplifler, implemented at miniaturized conflguration.