FIELD: engines and pumps.
SUBSTANCE: proposed engine comprises liquid or solid propellant fuel wherein oxidiser and/or combustible includes fixed nitrogen as well as fine or fixed boron. Note here that boron atoms-to-nitrogen atoms ratio makes 1:1 with departure of ±20%. Rocket fuel has fuel excess relative to oxidiser.
EFFECT: higher fuel heat generation.
9 cl
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET PROPELLANT /VERSIONS/ | 2014 |
|
RU2582712C2 |
| STAROVEROV'S PROPELLANT - 3 (VERSIONS) | 2014 |
|
RU2570012C1 |
| STAROVEROV'S PROPELLANT-6 | 2014 |
|
RU2570010C2 |
| STAROVEROV'S ROCKET ENGINE-6 (VERSIONS) | 2012 |
|
RU2570913C2 |
| METHOD FOR IMPROVING PROPELLANTS AND PROPELLANT (VERSIONS) | 2014 |
|
RU2570022C1 |
| STAROVEROV(S-18 ROCKET PROPELLANT /VERSIONS/ | 2014 |
|
RU2576857C2 |
| OXIDISER AND THEREOF-CONTAINING PROPELLANT | 2012 |
|
RU2534533C2 |
| ROCKET PROPELLANT | 2012 |
|
RU2513850C2 |
| STAROVEROV'S PROPELLANT - 17 (VERSIONS) | 2014 |
|
RU2572886C1 |
| JET PROPELLANT (VERSIONS) | 2012 |
|
RU2547476C2 |
