Theoretical Performance of Rocket Engines Using Gaseous Hydrogen in the Ideal State at Stagnation Temperatures Up to 200,000 R PDF Download

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Theoretical Performance of Rocket Engines Using Gaseous Hydrogen in the Ideal State at Stagnation Temperatures Up to 200,000 R

Theoretical Performance of Rocket Engines Using Gaseous Hydrogen in the Ideal State at Stagnation Temperatures Up to 200,000 R PDF Author: Richard Roback
Publisher:
ISBN:
Category : Hydrogen
Languages : en
Pages : 228

Book Description

Theoretical Performance of Rocket Engines Using Gaseous Hydrogen in the Ideal State at Stagnation Temperatures Up to 200,000 R

Theoretical Performance of Rocket Engines Using Gaseous Hydrogen in the Ideal State at Stagnation Temperatures Up to 200,000 R PDF Author: Richard Roback
Publisher:
ISBN:
Category : Hydrogen
Languages : en
Pages : 228

Book Description

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