Specific Impulse (Isp)
Glossary term: Specific Impulse (Isp)
01 Executive_Summary
A measure of rocket propulsion efficiency, defined as thrust divided by propellant mass flow rate. Higher Isp means less propellant for a given delta-v. Fusion propulsion concepts target Isp of 10⁴-10⁶ seconds.
02 Definition
A measure of rocket propulsion efficiency, defined as thrust divided by propellant mass flow rate. Higher Isp means less propellant for a given delta-v. Fusion propulsion concepts target Isp of 10⁴-10⁶ seconds.
03 Deep_Dive_Intelligence
Overview
A measure of rocket propulsion efficiency, defined as thrust divided by propellant mass flow rate. Higher Isp means less propellant for a given delta-v. Fusion propulsion concepts target Isp of 10⁴-10⁶ seconds.
Role: Glossary term: Specific Impulse (Isp)
Entity Type: Concept — Specific Impulse (Isp) is a technical concept or theoretical framework.
Technical Definition
A measure of rocket propulsion efficiency, defined as thrust divided by propellant mass flow rate. Higher Isp means less propellant for a given delta-v. Fusion propulsion concepts target Isp of 10⁴-10⁶ seconds.
Related Concepts: Fusion Driven Rocket, Plasma Propulsion
07 Key_Findings
- ▸ Role: Glossary term: Specific Impulse (Isp)
- ▸ Entity Type: Concept — Specific Impulse (Isp) is a technical concept or theoretical framework.
- ▸ Related Concepts: Fusion Driven Rocket, Plasma Propulsion
10 FAQ
What is Specific Impulse (Isp)? ▾
What does the deep dive analysis reveal about Specific Impulse (Isp)? ▾
External_References 5 REFS
Glossary_Sources
Type: concept
Region: glossary
Last updated: 2026-08-09