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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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In this part, the state of the art for several propulsion system components is reviewed, and some of the important factors which must be considered during the design of a supersonic propulsion system are pointed out. The discussion will be centered around the Mach number 3 cruise airplane of part III and the multimission airplane of part II.
Mariner 1969 multimission high rate deep space telemetry system design, hardware and application
Multimission solar electric spacecraft of modest size and variable propellant loading for interchangeable space missions - Vol. 1A
Multimission solar electric spacecraft for interchangeable space missions final technical systems data - Vol. 1B
Multimission solar electric spacecraft for interchangeable space missions program plans and cost estimates - Vol. 2
Multimission solar electric spacecraft for interchangeable interplanetary missions - Final summary technical report
Conceptual definition of reusable space shuttle systems with multimission capability - Vol. 1
Final vehicle configurations of reusable space shuttle systems with multimission capability - Vol. 2
Initial vehicle spectrum and parametric excursions of reusable space shuttle systems having multimission capability - Vol. 3
Technical analysis and performance of reusable space shuttle systems having multimission capability - Vol. 4
Subsystems and weight analysis of reusable space shuttle systems having multimission capability - Vol. 5
Propulsion analysis and tradeoffs for reusable space shuttle systems having multimission capability - Vol. 6
Integrated electronics for reusable space shuttle system having multimission capability - Vol. 7
Mission-payload and safety-abort analyses for reusable space shuttles with multimission capability - Vol. 8
Ground turnaround operations and facility requirements for reusable space shuttle systems having multimission capability - Vol. 9
Program development, cost analysis, and technology requirements for reusable space shuttle systems having multimission capability - Vol. 10
Tracking and data system support with multimission and high rate telemetry systems for the Mariner Mars 1969 project
Versatile, multimission solar electric propulsion upper stage for high energy, unmanned interplanetary flights - summary